Relevant bibliographies by topics / Conceptual Stage of Design

Academic literature on the topic 'Conceptual Stage of Design'

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Published: 6 September 2023

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Journal articles on the topic "Conceptual Stage of Design"

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OMURA, Masaru. "3204 Design Education at Conceptual Design Stage." Proceedings of Design & Systems Conference 2001.11 (2001): 296–97. http://dx.doi.org/10.1299/jsmedsd.2001.11.296.

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Zou, Jun Yan. "The Conceptual Design of Table Jaw Based on Functional Principle Design." Advanced Materials Research 605-607 (December 2012): 371–75. http://dx.doi.org/10.4028/www.scientific.net/amr.605-607.371.

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Mechanical product’s design can be divided into four stages that is task clarification, conceptual design, practical design and detailed design. The conceptual design is the most important and innovative stage of the four design stages. This paper deals with functional analysis and solutions of a table jaw and its conceptual design based on the theory of functional principle design. An innovative design method of a mechanical product is also discussed by means of functional principle design.
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Desai, Sumit, Shankar Mantha, and Vikas Phalle. "TRIZ and AHP in Early Design Stage of a Novel Reconfigurable Wheelchair." Journal of Mechanical Engineering 16, no. 3 (December 31, 2019): 123–41. http://dx.doi.org/10.24191/jmeche.v16i3.15352.

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The Reconfigurable wheelchair incorporated with sit-to-stand and sit-to-sleep capabilities is the technological solution for extensive wheelchair users to promote their quality of life (QoL), safety and comfort. This paper presents the conceptual design of a reconfigurable wheelchair using the TRIZ and AHP integrated approach. The objective of this study was to develop optimal conceptual designs of a reconfigurable wheelchair by overcoming identified design conflicts. The TRIZ contradiction toolkit was employed in the early conceptual design phase. Based on the TRIZ inventive principles and developed design strategy, new reconfigurable wheelchair mechanism was modelled in SolidWorks environment, using a top-down modelling approach. Dimensions of a wheelchair were kept within the dimensions of a standard wheelchair. The newly modelled mechanism was refined using motion simulation capabilities of the SolidWorks software. The new mechanism was further integrated with different wheelchair design features by means of the morphological chart in order to get innovative conceptual designs. Further, Analytical Hierarchy Process (AHP) was utilized as a multi-criteria decision making technique for optimal conceptual design selection. Conceptual design-I (joystick controller with electric drive) received highest weight among all conceptual designs, hence selected as the optimal conceptual design. Consistency ratio (CR) for the pair-wise comparisons made throughout the AHP method was found less than 0.10. All AHP calculations were supported by Microsoft Excel Add-in for multi-criteria decision problems. For the purpose of functionality testing of newly modelled wheelchair, 3D printed wheelchair parts have been fabricated (using ABS material) and tested for desired mechanical movements. The methodology implemented in the present work can be utilized for upcoming applications in design of new assistive devices.
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Chen, Xiao Chuan, Xiao Xia Lai, and John K. Gershenson. "Relative Design Cost Estimation at Design Stage Based on Design Features." Applied Mechanics and Materials 26-28 (June 2010): 625–36. http://dx.doi.org/10.4028/www.scientific.net/amm.26-28.625.

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With the global financial crisis happened, companies and investors pay more attention to development expense. Development costs mainly include design cost at the design stage. We analyze the design process and extract many design factors in order to estimate design cost at the conceptual and embodiment design stage. A number of process-based design features that impact the design cost are considered. These design factors include: 1) the number of performances and constraints, 2) sub-functions level and relationships, and 3) solutions at the conceptual design stage. At the embodiment of the design stage the design factors include: 1) the number of parts and their relationships, 2) the types of materials, 3) load resources, and 4) the number and types of tolerances. We use relative cost to estimate design cost by comparing the number of design factors among designs. To demonstrate the relative design cost estimation in practice, Kodak single-use cameras are used as example products. Use of these methods proves beneficial in estimate design cost in the design process.
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Cui, Yu Lian, and Wei Wu. "A Review of Reliability Principles in Conceptual Design." Advanced Materials Research 199-200 (February 2011): 583–86. http://dx.doi.org/10.4028/www.scientific.net/amr.199-200.583.

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In this paper an attempt has been made to identify certain useful parts that will assist to consider reliability during conceptual design phase. The aim is to provide some thoughts and a toolkit for addressing reliability during the early stages of design, influencing design decisions and product reliability, and reducing the relying on the reliability prediction and expensive experiments in later design stage. Therefore high reliability can be cost-effectively achieved.
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Lee, Kyung-Jae, Sang-Hun Kang, Soo-Seok Yang, and Chul Park. "Conceptual Design Study of Two-Stage Hypersonic Scramjet Vehicle." Journal of the Korean Society of Propulsion Engineers 16, no. 1 (February 1, 2012): 16–24. http://dx.doi.org/10.6108/kspe.2012.16.1.016.

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Sayli, Ayla, Ahmet Dursun Alkan, Radoslav Nabergoj, and Ayse Oncu Uysal. "Seakeeping assessment of fishing vessels in conceptual design stage." Ocean Engineering 34, no. 5-6 (April 2007): 724–38. http://dx.doi.org/10.1016/j.oceaneng.2006.05.003.

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Houseman, Oliver, Rajkumar Roy, Charles Wainwright, and Evaggelos Lavdas. "Cost optimising aircraft systems at a conceptual design stage." International Journal of Manufacturing Technology and Management 15, no. 3/4 (2008): 328. http://dx.doi.org/10.1504/ijmtm.2008.020174.

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Bardenhagen, Andreas, and Dmitry Rakov. "ADVANCED MORPHOLOGICAL APPROACH IN AEROSPACE DESIGN DURING CONCEPTUAL STAGE." Facta Universitatis, Series: Mechanical Engineering 17, no. 3 (November 29, 2019): 321. http://dx.doi.org/10.22190/fume180110005b.

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This paper presents an advanced morphological approach supporting designers and developers in their search for as well as synthesis and analysis of new engineering solutions during the conceptual design stage. The proposed method is based on the cluster analysis and the set theory, the set of rules and engineering implementations maximizing the gain of the products potential. The number of possible combinations using the standard morphological technology is extremely large. We present a mathematical framework that handles this problem. The method was evaluated with case studies of new engineering solutions in aerospace, ecology and adaptive soundproofing system. The case studies verified the significant potential of the proposed approach in comparison with the methods presently in use.
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Lou, Xi Yin. "Research on Conceptual Design of Green Electromechanical Products." Advanced Materials Research 904 (March 2014): 414–16. http://dx.doi.org/10.4028/www.scientific.net/amr.904.414.

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The concept design of green products is according to the various phases of the product life cycle, product function to create and functional decomposition, to meet the principle of solving functional requirements and Realization of the idea and the system design principle of vector scheme of function structure. The conceptual design process is a process of divergent thinking and innovative design, the optimal process plan. Therefore, the conceptual design stage is a very innovative design stage, is also the green design is the most important stage.
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Dissertations / Theses on the topic "Conceptual Stage of Design"

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Agarwal, Pranab. "Conceptual design of long-span trusses using multi-stage heuristics." Thesis, Texas A&M University, 2003. http://hdl.handle.net/1969.1/3863.

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A hybrid method that addresses the design and optimization of long-span steel trusses is presented. By utilizing advancements in present day computing and biologically inspired analysis and design, an effort has been made to automate the process of evolving optimal trusses in an unstructured problem domain. Topology, geometry and sizing optimization of trusses are simultaneously addressed using a three stage methodology. Multi-objective genetic algorithms are used to optimize the member section sizes of truss topologies and geometries. Converting constraints into additional objectives provides a robust algorithm that results in improved convergence to the pareto-optimal set of solutions. In addition, the pareto-curve plotted based on how well the different objectives are satisfied helps in identifying the trade-offs that exist between these objectives, while also providing an efficient way to rank the population of solutions during the search process. A comparison study between multi-objective genetic algorithms, simulated annealing, and reactive taboo search is conducted to evaluate the efficiency of each method with relation to its overall performance, computational expense, sensitivity to initial parameter settings, and repeatability of finding near-global optimal designs. The benefit of using a three stage approach, and also implementing the entire model on parallel computers, is the high level of computational efficiency that is obtained for the entire process and the near-optimal solutions obtained. The overall efficiency and effectiveness of this method has been established by comparing the truss design results obtained using this method on bridge and roof truss benchmark problems with truss designs obtained by other researchers. One of the salient features of thisresearch is the large number of optimal trusses that are produced as the final result. The range of designs available provides the user with the flexibility to select the truss design that best matches their design requirements. By supporting human-computer interactions between these stages, the program also incorporates subjective aesthetic criteria, which assist in producing final designs in consonance with the user's requirements.
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Sigvant, John. "Conceptual Design of an Air- launched Multi-stage Launch Vehicle." Thesis, KTH, Fysik, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-284355.

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In the present thesis, the objective was to find the maximum amount of payload mass that can be put into a 500 km polar orbit by a 1400 kg air-launched multi-stage rocket launched from a fighter jet platform. To fulfill the objective an algorithm incorporating several modules was developed. The modules performed calculations based on theoretical models and literature values to arrive at optimal design variables. From the design the maximum payload mass was able to be derived and it was concluded that a three-stage launch vehicle was able to deliver a 22.0 kg payload to the desired orbit.
I den här avhandlingen var syftet att hitta den maximala mängden nyttolastmassa som kan transporteras av en 1400 kg flerstegsraket uppskjuten från luften till en 500 km polär bana. För att uppfylla målet utvecklades en algoritm med flera moduler. Modulerna utförde beräkningar baserade på teoretiska modeller och litteraturvärden för att komma fram till optimala designvariabler. Från konstruktionen kunde den maximala nyttolastmassan härledas och det konstaterades att en trestegsraket kunde leverera en nyttolast på 22.0 kg till den önskade omloppsbanan.
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Ballard, Claire. "Conceptual lay-out of small launcher." Thesis, KTH, Energiteknik, 2012. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-95206.

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The objective of this diploma thesis is to perform a conceptual lay-out of a small launcher. Re- quirements have been defined in order to realize this first preliminary study and design of a small launcher. In that frame, a MATLAB code has been written in order to simulate the rocket tra- jectories. An optimization program on launcher staging has been written as well. To validate this code, the VEGA and Ariane 5 launchers have been used. Then from studies on existing launchers, simulations have been performed in order to find an optimum small launcher and later on to design more precisely the small launcher. As a requirement an upper stage has been newly designed for the purpose of the study. At the end, two small launchers have been considered: a three-stage launcher using the Zefiro 23 as a first stage, the Zefiro 9 as a second stage, and an upper stage using a 3kN thrust engine; a two-stage launcher using the Zenit booster engine in the first stage, and an upper stage using a 22kN thrust engine.
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Mustafa, Janan Abdulsattar. "Computer-based sketching and the productivity of the conceptual stage of design." Thesis, University of Edinburgh, 2013. http://hdl.handle.net/1842/8858.

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Many designers find computer-based tools are not as effective during the early stages of design as manual sketching. However, to abandon the computer in these conceptual stages denies designers the computer‟s capability to translate and supplement imaginative design thinking. Recent design studies address conceptual design. What is the impact of computer-based drawing and sketching on designers‟ cognition and productive reasoning? This research focuses on the relationship between the characteristics of sketching using the drawing environment of the computer and the productivity of the conceptual design phase. I provide a theoretical framework that identifies and clarifies both sketching and productivity. Previous specialized studies are selective and sometimes only descriptive in defining this relationship. A review of these studies reveals a gap in our understanding of those aspects of sketching that relate to visualization, imagination and the generation of design ideas. The thesis addresses three objectives: (i) to build a comprehensive theoretical framework that on one hand defines the characteristics of sketching that might affect the generation of design ideas, and on the other hand defines the productivity of conceptual design and its indicators; (ii) to apply this framework in a practical study; and (iii) to extract implications for the relationship. To address the problem of computer-based sketching, I indentify the continuity within the dynamic field of images usually generated while designers sketch as the most effective characteristic of the computer sketching process. I establish a measure of continuity defined by (i) the degree of ease in projecting design images, (ii) the degree of continuity of displaying images due to changing the status of the design objects and due to navigation around the objects, (iii) the degree of provision of a holistic view (i.e., the total view of the design objects on the computer screen). Then I define productivity within this framework in terms of the cognitive operations of dialogical reinterpretation. When sketching, designers seem to perform key operations such as interpreting, reframing and restructuring. I present the case that a process rich with these cognitive operations is productive. The study makes use of the fields of free hand sketching, literature, cognitive psychology and Gestalt theory. Four indicators emerge from this study: the occurrence of pattern discovery, conceptual reinterpretation, alternation of thinking, and restructuring. I identify key variables that define the degree of continuity of the dynamic field of images which relate to designer‟s performance to verify their relationship with productivity. I study ten design participants who are given a design task that involves sketching with various CAD systems. The study involves 21 hours of recorded video analyzed using a method adapted from Goldschmidt's “linkography” tool for representing design protocols. I identify where patterns of relationships between variables exist, and where they do not apply. Not all the selected variables of continuity of the dynamic field of images, nor all the indicators of productivity in the conceptual design phase, support these patterns of relationships. This indicates that there is a special group of characteristics of sketching that maintain the pace of continuity within the dynamic field of images can improve the productivity in the conceptual phase.
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Lejon, Alexander. "Creation and Validation of Early Stage Conceptual Design Methodology for Blended WingBody Aircraft." Thesis, KTH, Flygdynamik, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-261700.

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The current design paradigm for developing tube-and-wing style aircraft has been well documented in literature. This research attempts to develop and val-idate a similar design methodology to what is presently utilized for tube-and-wing based aircraft, but has so far not been successfully implemented for the blended wing-body. This construction has no clear distinction between the lift generating surfaces and the cargo carrying structure. The methodology that was developed included the concatenation and validation of low-fidelity, low speed and low complexity aerodynamic models in order to allow for quick and simple analysis of a large number of possible geometries. This enables the user eÿciently determine the most promising candidate geometries for further study and/or development. Known issues with the low velocity and low com-plexity aerodynamic models include the absence of shock wave modelling, an important part in determining the aerodynamic performance of a lift generat-ing surface. The result of this work is the creation and documentation of a procedure for early-stage design of a blended wing-body airframe. However, due to convergence issues with the high-fidelity CFD solver, the methodology could not been validated for transonic flow. It can thus be only considered valid for flow velocities for which the Prandtl-Glauert correction is valid.
Den befintliga konstruktionsmetodiken för utveckling och design av flygfarkoster är väl dokumenterad i tidigare publicerad litteratur. Detta arbete ämmar utveckla och validera en liknande metodologi som redan existerar för de väl etablerade flygplansgeometrier som baseras på cylinder/vingar-principen. Metoden som utvecklades inkluderade sammansättaning och validering av tidigare existerande lågupplösta samt lågkomplexa aerodynamiska modeller avsedda för beräkning av flödesekvationer för inkompressibel, friktionsfri och stationär strömning. Detta var avsett att möjliggöra ögonblicksvalidering av en föreslagen sammansmält kropp/vinge-geometri med speciell fokus på vissa prestationsbaserade nyckeltal. För cylinder/vinge-geometrier är dessa lågupplösta metoder i litteraturen väletablerat inexakta på grund av en avsaknad av stötvågsmodellering, men då stora delar av de lyftkraftsgenererande ytorna för-ändrats på en sammansmält kropp/vinge är inte nödvändigtvis detta sant för den typen av flygplan också. Då de högupplösta, mer komplexa höghastighetssimuleringarna inte konvergerade inom den utsatta tiden kan den föreslagna metodiken endast anses giltig för det intervall av flödeshastighet vari PrandtlGlauerts korrektionsfaktor stämmer väl överens med verkligheten.
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Al-Dosary, Bashar. "Integrating 3D-CAD and Cost Estimating at the Conceptual Design Stage of Bridge Project." Thesis, Université d'Ottawa / University of Ottawa, 2015. http://hdl.handle.net/10393/32570.

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Bridge Information Modeling (BrIM), as a concept, has been introduced to enhance the procedures of the whole phases of a bridge life-cycle starting with concept and design, through construction and operation, and ending with maintenance and rehabilitation. Integrating BrIM and design tools will help improve the methods used in designing and constructing bridge projects at early stages taking into considerations their cost and time constraints. The main objective of this research is to develop an integrated model that helps owners, designers and construction managers visualize bridge projects in a 3D mode and accordingly automate the process of generating preliminary cost estimates during the conceptual design stage. To achieve the above mentioned objective, a proposed methodology will be applied where all the aspects needed to develop an efficiently integrated model are realized. Thus, this research describes the proposed methodology that incorporates three modules, which are the core of the integrated model. These modules are: a knowledge based system module, which is used to generate conceptual dimensions and parameters depending on algorithmic and heuristic knowledge gathered from codes, guidelines and design experts; a conceptual cost estimation module, which is used to generate conceptual cost estimate based on the results of the first module; and a 3DCAD module, which is integrated with the previous modules where users will visualize the proposed bridge in 3D based on the results of the knowledge based module. The successful development of the model would help owners and investors identify the cost and visualize the proposed projects at the early stages of the project life, so they have an idea of the budget required and the aesthetics of the proposed projects. The integrated model is validated through an actual case project to test its workability and output.
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Osti, Francesco. "Tecniche innovative di modellazione diretta nell'early stage design." Master's thesis, Alma Mater Studiorum - Università di Bologna, 2016.

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Partendo da un’analisi dei problemi che si incontrano nella fase di conceptual design, si presentano le diverse tecniche di modellazione tridimensionale, con particolare attenzione al metodo subdivision e agli algoritmi che lo governano (Chaikin, Doo – Sabin). Vengono poi proposti alcuni esempi applicativi della modellazione free form e skeleton, con una successiva comparazione, sugli stessi modelli, delle sequenze e operazioni necessarie con le tradizionali tecniche di modellazione parametrica. Si riporta un esempio dell’utilizzo del software IronCAD, il primo software a unire la modellazione parametrica e diretta. Si descrivono le limitazioni della modellazione parametrica e di quella history free nella fase concettuale di un progetto, per arrivare a definire le caratteristiche della hybrid modeling, nuovo approccio alla modellazione. Si presenta brevemente il prototipo, in fase di sviluppo, che tenta di applicare concretamente i concetti dell’hybrid modeling e che vuole essere la base di partenza per una nuova generazione di softwares CAD. Infine si presenta la possibilità di ottenere simulazioni real time su modelli che subiscono modifiche topologiche. La simulazione real time è permessa dalla ridefinizione in forma parametrica del problema lineare elastico che viene successivamente risolto mediante l’applicazione congiunta delle R – Functions e del metodo PGD. Seguono esempi di simulazione real time.
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Babak, I., and E. Druzhinin. "Computer-Aided Design System Application at Conceptual Stage of Unmanned Air Vehicle Life Cycle." Thesis, Sumy State University, 2016. http://essuir.sumdu.edu.ua/handle/123456789/47035.

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The steps of computer-aided design system application at conceptual stage of unmanned air vehicle life cycle are considered. Sequential and iterative approach to an aircraft design process are compared.
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Hosseinipour, Milad. "Design and Development of an Intra-Ventricular Assistive Device For End Stage Congestive Heart Failure Patients: Conceptual Design." University of Toledo / OhioLINK, 2013. http://rave.ohiolink.edu/etdc/view?acc_num=toledo1372726495.

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Rivera, Rosario. "An empirical study of the conceptual stage of design in mechanical engineering and its implications for CAD." Thesis, University of Wolverhampton, 1996. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.309581.

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Books on the topic "Conceptual Stage of Design"

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United States. National Aeronautics and Space Administration., ed. Conceptual design of two-stage-to-orbit hybrid launch vehicle. [Cleveland, Ohio]: Case Western Reserve University, 1991.

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United States. National Aeronautics and Space Administration., ed. Conceptual design of two-stage-to-orbit hybrid launch vehicle. [Cleveland, Ohio]: Case Western Reserve University, 1991.

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Andreasen, Mogens Myrup, Claus Thorp Hansen, and Philip Cash. Conceptual Design. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-19839-2.

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O'Sullivan, Barry. Constraint-aided conceptual design. London: Professional Engineering, 2002.

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Howe, Denis. Aircraft Conceptual Design Synthesis. Chichester, UK: John Wiley & Sons, Ltd, 2000. http://dx.doi.org/10.1002/9781118903094.

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French, M. J. Conceptual Design for Engineers. Berlin, Heidelberg: Springer Berlin Heidelberg, 1985. http://dx.doi.org/10.1007/978-3-662-11364-6.

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Sully, Anthony. Interior Design: Conceptual Basis. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-16474-8.

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French, Michael J. Conceptual Design for Engineers. London: Springer London, 1999. http://dx.doi.org/10.1007/978-1-4471-3627-9.

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Stecklein, J. M. Lunar lander conceptual design. [S.l.]: [s.n.], 1988.

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Hollowell, Steven James. Conceptual design optimization study. Hampton, Va: Langley Research Center, 1990.

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Book chapters on the topic "Conceptual Stage of Design"

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Tizani, Walid. "Collaborative Design in Virtual Environments at Conceptual Stage." In Collaborative Design in Virtual Environments, 67–76. Dordrecht: Springer Netherlands, 2011. http://dx.doi.org/10.1007/978-94-007-0605-7_6.

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Shieh, Win-Bin, and Ching-Kong Chen. "Conceptual Design of a Two-Stage Variable Gravity Compensated Mechanism." In Advances in Mechanism and Machine Science, 1535–43. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-20131-9_152.

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Acharya, Shakuntala, and Amaresh Chakrabarti. "‘ConcepTe’: Supporting Environmentally Benign Design Decision-Making at Conceptual Stage." In Smart Innovation, Systems and Technologies, 335–44. Singapore: Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-5974-3_29.

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Wu, H. J., L. C. Shih, and C. H. Ding. "A Dialogue Module at the Conceptual Product Design Stage through Genetic Algorithm." In Soft Computing in Engineering Design and Manufacturing, 306–9. London: Springer London, 1998. http://dx.doi.org/10.1007/978-1-4471-0427-8_33.

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Mishra, Samaresh, Elina Aisuryalaxmi, and Rajib Mall. "Estimating Database Size and Its Development Effort at Conceptual Design Stage." In Communications in Computer and Information Science, 120–27. Berlin, Heidelberg: Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-29216-3_14.

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Chiba, Kazuhisa, Masahiro Kanazaki, Koki Kitagawa, and Toru Shimada. "Conceptual Design of Single-Stage Launch Vehicle with Hybrid Rocket Engine Using Design Informatics." In Computational Methods in Applied Sciences, 369–84. Cham: Springer International Publishing, 2014. http://dx.doi.org/10.1007/978-3-319-11541-2_24.

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Rakov, Dmitry. "Business Information Systems for Innovative Projects Evaluation at the Conceptual Design Stage." In Advances in Intelligent Systems, Computer Science and Digital Economics III, 138–49. Cham: Springer International Publishing, 2022. http://dx.doi.org/10.1007/978-3-030-97057-4_13.

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Rodgers, Paul, Alistair Patterson, and Derek Wilson. "A Formal Method for Assessing Product Performance at the Conceptual Stage of the Design Process." In Advances in Formal Design Methods for CAD, 137–64. Boston, MA: Springer US, 1996. http://dx.doi.org/10.1007/978-0-387-34925-1_8.

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Hall, Roy. "Supporting Complexity and Conceptual Design in Modeling Tools." In State of the Art in Computer Graphics, 153–83. New York, NY: Springer New York, 1991. http://dx.doi.org/10.1007/978-1-4612-4448-6_7.

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Hernández-Montes, Agustín Job, Guillermo Cortés-Robles, Giner Alor-Hernández, and Jorge Luis García-Alcaraz. "The Use of Affective Computing in the Conceptual Design Stage of New Products." In Management and Industrial Engineering, 207–28. Cham: Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-93716-8_10.

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Conference papers on the topic "Conceptual Stage of Design"

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Galchynska, O. S., and R. A. Cheremskyi. "CONCEPTUAL DESIGN: THE INITIAL STAGE OF PRODUCT DESIGN." In АКТУАЛЬНІ ПРОБЛЕМИ РОЗВИТКУ УКРАЇНСЬКОГО ТА ЗАРУБІЖНОГО МИСТЕЦТВ: КУЛЬТУРОЛОГІЧНИЙ, МИСТЕЦТВОЗНАВЧИЙ, ПЕДАГОГІЧНИЙ АСПЕКТИ. Liha-Pres, 2023. http://dx.doi.org/10.36059/978-966-397-317-3-70.

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Hur, Doe Young, Min-ho Kwak, Su-Hwan Yoon, and Dongho Lee. "Aerodynamic Optimization on the Conceptual Design Stage." In 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2011. http://dx.doi.org/10.2514/6.2011-9.

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KIM, DAVID, JOSEPH ADAMS, C. GRANT, INKI MIN, and JASON CHIANG. "Advanced upper stage, a conceptual upper stage design for ALS." In 26th Joint Propulsion Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-2701.

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Parkinson, Alan, Kenneth Chase, and Matt Rogers. "Robust Design via Tolerance Analysis in the Conceptual Design Stage." In ASME 1999 Design Engineering Technical Conferences. American Society of Mechanical Engineers, 1999. http://dx.doi.org/10.1115/detc99/dac-8577.

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Abstract Robust design methods are used to develop designs which can tolerate variation. Most methods developed to date are applied during the detailed design phase. Yet the potential for developing robust designs is greatest during the conceptual design stage, where the overall design concept is determined. This research is part of a larger effort to develop robust design methods for conceptual design. The focus of the research is on developing methods for identifying critical tolerances during concept evaluation. We propose that in many mechanical designs, a 70-30 rule applies: 30% of the tolerances contribute 70% of the variation. This hypothesis is supported by the results from several case studies. We discuss progress in developing methods — in particular the vector loop method — which can be applied during conceptual design to detect critical tolerances. By being aware of these tolerances early in the design process, the designer can either change the design to make the tolerances less critical or make sure the tolerances are appropriately considered as manufacturing process plans are developed.
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Sieger, David B., and Reino E. Salmi. "Conceptual Design Tool for the Systematic Design Method." In ASME 1997 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 1997. http://dx.doi.org/10.1115/imece1997-0014.

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Abstract The significance of activities performed during the initial design process stages suggests the need for supporting computer applications. Currently, such support is not available until the detailed design stage is reached. Although several models addressing activities occurring prior to this stage appear in the literature, these models are limited in their ability to be scaled up to real-world problems, integrated with existing tools, and/or provide guidance to participants. A window-based application for the conceptual design stage that effectively addresses these limitations is presented in this paper. Our approach is unique in that it combines existing methodologies for function and system decomposition in a way not previously considered, as well as facilitating the use of a design guidance mechanism. An example demonstrating the use of the resulting tool to a conceptual design problem is provided.
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Linna Zhu. "User research at the maturity stage of product lifecycle." In 2009 IEEE 10th International Conference on Computer-Aided Industrial Design & Conceptual Design. IEEE, 2009. http://dx.doi.org/10.1109/caidcd.2009.5375313.

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Weiss, Marco, and Niclas M. Dzikus. "An Airport Assessment Approach in the Conceptual Design Stage." In 15th AIAA Aviation Technology, Integration, and Operations Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2015. http://dx.doi.org/10.2514/6.2015-3185.

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Yang, Inyoung, Chul Park, Sangmin Choi, and Soo-Seok Yang. "Conceptual Design of Short-Range Two-Stage Scramjet Vehicle." In 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2011. http://dx.doi.org/10.2514/6.2011-502.

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Al-Khaledi, Sadoun Mater, and Mohammed Majeed. "Developing High H2S Facility Design Requirements In Conceptual Stage." In SPE Kuwait International Petroleum Conference and Exhibition. Society of Petroleum Engineers, 2012. http://dx.doi.org/10.2118/163349-ms.

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Zuo, J., and S. Director. "An integrated design environment for early stage conceptual design (poster paper)." In the conference. New York, New York, USA: ACM Press, 2000. http://dx.doi.org/10.1145/343647.344150.

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Reports on the topic "Conceptual Stage of Design"

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Sedano, Nils M., Jonathan Painter, and Ray Walsh. Conceptual Design, Feasibility and Payoff Analysis of a Third Stage for EELV. Fort Belvoir, VA: Defense Technical Information Center, June 2014. http://dx.doi.org/10.21236/ada611030.

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Sedano, Nils M., Jonathan Painter, and Ray Walsh. Conceptual Design, Feasibility and Payoff Analysis of a Third Stage for EELV (Briefing Charts). Fort Belvoir, VA: Defense Technical Information Center, July 2014. http://dx.doi.org/10.21236/ada618201.

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Abrams, L. M., A. G. Comolli, G. A. Popper, C. Wang, and G. Wilson. Low-severity catalytic two-stage liquefaction process: Illinois coal conceptual commercial plant design and economics. Office of Scientific and Technical Information (OSTI), September 1988. http://dx.doi.org/10.2172/6431773.

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Kaliuga, V. V., A. V. Trifanov, V. I. Bazykin, and E. A. Tikhonov. Substantiation of a two-phase stress-free way of keeping pigs at the stage of conceptual design of pig farms. Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования Ивановская государственная сельскохозяйственная академия им. акад. Д.К. Беляева, 2018. http://dx.doi.org/10.18411/0131-5226-2018-11994.

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Trifanov, A. V., V. V. Kaliuga, and V. I. Bazykin. Investigation of the characteristics of a four-phase stress-free way of keeping pigs at the conceptual design stage of small pig farms. Федеральное государственное бюджетное научное учреждение "Федеральный научный агроинженерный центр ВИМ" (ФГБНУ ФНАЦ ВИМ), 2018. http://dx.doi.org/10.18411/0131-5226-2018-11995.

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ROBINSON, K. CONCEPTUAL DESIGN REPORT. Office of Scientific and Technical Information (OSTI), December 2006. http://dx.doi.org/10.2172/910923.

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Peretz, F. J. Conceptual design summary. Office of Scientific and Technical Information (OSTI), September 1992. http://dx.doi.org/10.2172/7282459.

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Peretz, F. J. Conceptual design summary. Office of Scientific and Technical Information (OSTI), September 1992. http://dx.doi.org/10.2172/10174831.

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Nagamiya, Shoji, Samuel H. Aronson, Glenn R. Young, and Leo Paffrath. PHENIX Conceptual Design Report. Office of Scientific and Technical Information (OSTI), January 1993. http://dx.doi.org/10.2172/6370496.

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Abrams, R. J. Mu2e Conceptual Design Report. Office of Scientific and Technical Information (OSTI), March 2012. http://dx.doi.org/10.2172/1398490.

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