Relevant bibliographies by topics / Active aerodynamics

Academic literature on the topic 'Active aerodynamics'

Author: Grafiati
Published: 4 June 2021
Last updated: 1 February 2022

Create a spot-on reference in APA, MLA, Chicago, Harvard, and other styles

Select a source type:

Contents

Consult the lists of relevant articles, books, theses, conference reports, and other scholarly sources on the topic 'Active aerodynamics.'

Next to every source in the list of references, there is an 'Add to bibliography' button. Press on it, and we will generate automatically the bibliographic reference to the chosen work in the citation style you need: APA, MLA, Harvard, Chicago, Vancouver, etc.

You can also download the full text of the academic publication as pdf and read online its abstract whenever available in the metadata.

Journal articles on the topic "Active aerodynamics"

1

Kurec, Krzysztof, Michał Remer, Jakub Broniszewski, Przemysław Bibik, Sylwester Tudruj, and Janusz Piechna. "Advanced Modeling and Simulation of Vehicle Active Aerodynamic Safety." Journal of Advanced Transportation 2019 (February 3, 2019): 1–17. http://dx.doi.org/10.1155/2019/7308590.

Full text
Abstract:
The aim of this study was to extend the safety limits of fast moving cars by the application, in a controlled way, of aerodynamic forces which increase as the square of a car’s velocity and, if left uncontrolled, dramatically reduce car safety. This paper presents the methods, assumptions, and results of numerical and experimental investigations by modeling and simulation of the aerodynamic characteristics and dynamics of a small sports car equipped with movable aerodynamic elements operated by an electronic subsystem for data acquisition and aerodynamics active automatic control.
APA, Harvard, Vancouver, ISO, and other styles
2

Žilinský, Juraj, and Milan Vanc. "Applied Aerodynamics in Building." Advanced Materials Research 855 (December 2013): 164–67. http://dx.doi.org/10.4028/www.scientific.net/amr.855.164.

Full text
Abstract:
Development of new materials, high strength concrete, steels, composites, new construction techniques and procedures put the Development of new materials, high strength concrete, steels, composites, new construction techniques and procedures put the foundations of a new generation of buildings. With the advent of advanced computer technology, using the finite element method engineers and architects plan and construct buildings that are, high, flexible, thin and lightweight. These buildings, however, are burdened by aerodynamic forces, whose source is wind. Just the action of aerodynamic forces adversely affects their ability to traffic, reducing safety and durability. It is therefore necessary to provide high flexibility structures and maintain their safety. This can only be achieved by means of applied aerodynamics using various types of passive and active components to optimize aerodynamics of buildings.
APA, Harvard, Vancouver, ISO, and other styles
3

Jung, Frank. ""All vehicles can benefit from active aerodynamics"." ATZ worldwide 123, no. 4 (March 26, 2021): 22–25. http://dx.doi.org/10.1007/s38311-021-0647-0.

Full text
APA, Harvard, Vancouver, ISO, and other styles
4

Althoff, Matthias, Mayuresh J. Patil, and Johannes P. Traugott. "Nonlinear Modeling and Control Design of Active Helicopter Blades." Journal of the American Helicopter Society 57, no. 1 (January 1, 2012): 1–11. http://dx.doi.org/10.4050/jahs.57.012002.

Full text
Abstract:
This paper presents the theoretical basis for the simulation and control of active helicopter blades. The analysis is based on a model that considers the structural dynamics, the aerodynamics, as well as the integrated blade actuation and sensing. The effect of the integral actuation enters the beam model via an active beam cross-sectional analysis. A two-dimensional incompressible, inviscid, quasi-steady aerodynamic model is coupled to the active structural model. For simulation, analysis, and control design, the blade model is discretized in space using a Galerkin approach. The resulting nonlinear model of high order is reduced using the aeroelastic modes of the blade. Finally, the usefulness of a reduced-order model is demonstrated by designing an energy optimal linear-quadratic-Gaussian (LQG) control.
APA, Harvard, Vancouver, ISO, and other styles
5

NIE, RUI, JINHAO QIU, HONGLI JI, and DAWEI LI. "AERODYNAMIC CHARACTERISTIC OF THE ACTIVE COMPLIANT TRAILING EDGE CONCEPT." International Journal of Modern Physics: Conference Series 42 (January 2016): 1660173. http://dx.doi.org/10.1142/s2010194516601733.

Full text
Abstract:
This paper introduces a novel Morphing Wing structure known as the Active Compliant Trailing Edge (ACTE). ACTE structures are designed using the concept of “distributed compliance” and wing skins of ACTE are fabricated from high-strength fiberglass composites laminates. Through the relative sliding between upper and lower wing skins which are connected by a linear guide pairs, the wing is able to achieve a large continuous deformation. In order to present an investigation about aerodynamics and noise characteristics of ACTE, a series of 2D airfoil analyses are established. The aerodynamic characteristics between ACTE and conventional deflection airfoil are analyzed and compared, and the impacts of different ACTE structure design parameters on aerodynamic characteristics are discussed. The airfoils mentioned above include two types (NACA0012 and NACA64A005.92). The computing results demonstrate that: compared with the conventional plane flap airfoil, the morphing wing using ACTE structures has the capability to improve aerodynamic characteristic and flow separation characteristic. In order to study the noise level of ACTE, flow field analysis using LES model is done to provide noise source data, and then the FW-H method is used to get the far field noise levels. The simulation results show that: compared with the conventional flap/aileron airfoil, the ACTE configuration is better to suppress the flow separation and lower the overall sound pressure level.
APA, Harvard, Vancouver, ISO, and other styles
6

Czyż, Zbigniew, and Mirosław Wendeker. "Measurements of Aerodynamic Interference of a Hybrid Aircraft with Multirotor Propulsion." Sensors 20, no. 12 (June 13, 2020): 3360. http://dx.doi.org/10.3390/s20123360.

Full text
Abstract:
This article deals with the phenomenon of aerodynamic interference occurring in the innovative hybrid system of multirotor aircraft propulsion. The approach to aerodynamics requires a determination of the impact of active sources of lift and thrust upon the aircraft aerodynamic characteristics. The hybrid propulsion unit, composed of a conventional multirotor source of thrust as well as lift in the form of the main rotor and a pusher, was equipped with an additional propeller drive unit. The tests were conducted in a continuous-flow low speed wind tunnel with an open measuring space, 1.5 m in diameter and 2.0 m long. Force testing made it possible to develop aerodynamic characteristics as well as defining aerodynamic characteristics and defining the field of speed for the considered design configurations. Our investigations enabled us to analyze the results in terms of a mutual impact of particular components of the research object and the area of impact of active elements present in a common flow.
APA, Harvard, Vancouver, ISO, and other styles
7

Qin, N., Y. Zhu, and S. T. Shaw. "Numerical study of active shock control for transonic aerodynamics." International Journal of Numerical Methods for Heat & Fluid Flow 14, no. 4 (June 2004): 444–66. http://dx.doi.org/10.1108/09615530410532240.

Full text
APA, Harvard, Vancouver, ISO, and other styles
8

Dowell, Earl H., Kenneth C. Hall, and Michael C. Romanowski. "Eigenmode Analysis in Unsteady Aerodynamics: Reduced Order Models." Applied Mechanics Reviews 50, no. 6 (June 1, 1997): 371–86. http://dx.doi.org/10.1115/1.3101718.

Full text
Abstract:
In this article, we review the status of reduced order modeling of unsteady aerodynamic systems. Reduced order modeling is a conceptually novel and computationally efficient technique for computing unsteady flow about isolated airfoils, wings, and turbomachinery cascades. Starting with either a time domain or frequency domain computational fluid dynamics (CFD) analysis of unsteady aerodynamic or aeroacoustic flows, a large, sparse eigenvalue problem is solved using the Lanczos algorithm. Then, using just a few of the resulting eigenmodes, a Reduced Order Model of the unsteady flow is constructed. With this model, one can rapidly and accurately predict the unsteady aerodynamic response of the system over a wide range of reduced frequencies. Moreover, the eigenmode information provides important insights into the physics of unsteady flows. Finally, the method is particularly well suited for use in the active control of aeroelastic and aeroacoustic phenomena as well as in standard aeroelastic analysis for flutter or gust response. Numerical results presented include: 1) comparison of the reduced order model to classical unsteady incompressible aerodynamic theory, 2) reduced order calculations of compressible unsteady aerodynamics based on the full potential equation, 3) reduced order calculations of unsteady flow about an isolated airfoil based on the Euler equations, and 4) reduced order calculations of unsteady viscous flows associated with cascade stall flutter, 5) flutter analysis using the Reduced Order Model. This review article includes 25 references.
APA, Harvard, Vancouver, ISO, and other styles
9

Bieler, Heribert. "Active flow control concepts and application opportunities." Aircraft Engineering and Aerospace Technology 89, no. 5 (September 4, 2017): 725–29. http://dx.doi.org/10.1108/aeat-01-2017-0015.

Full text
Abstract:
Purpose Aerodynamics drives the aircraft performance and, thus, influences fuel consumption and environmental compatibility. Further, optimization of aerodynamic shapes is an ongoing design activity in industrial offices; this will lead to incremental improvements. More significant step changes in performance are not expected from pure passive shape design. However, active flow control is a key technology, which has the potential to realize a drastic step change in performance. Flow control targets two major goals: low speed performance enhancements mainly for start and landing phase via control of separation and drag reduction at high speed conditions via skin friction and shock wave control. Design/methodology/approach This paper highlights flow control concepts and Airbus involvements for both items. To mature flow control systematically, local applications of separation control technology are of major importance for Airbus. In parallel, but at lower maturity level, investigations are ongoing to reduce the turbulent skin friction at cruise. A popular concept to delay separation at low speed conditions is the implementation of jet actuation control systems flush mounted to the wall of aerodynamic components. Findings In 2006, DLR (in collaboration with universities Berlin, Braunschweig and industrial partner Airbus) started to study active flow control for separation delay towards application. Based on basic proof of concepts (achieved in national projects), further flow control hardware developments and wind tunnel and lab testing took place in European funded projects. Originality/value Significant lift enhancements were realized via flow control applied to the wing leading edge and the flap.
APA, Harvard, Vancouver, ISO, and other styles
10

Psiaki, Mark L. "Nanosatellite Attitude Stabilization Using Passive Aerodynamics and Active Magnetic Torquing." Journal of Guidance, Control, and Dynamics 27, no. 3 (May 2004): 347–55. http://dx.doi.org/10.2514/1.1993.

Full text
APA, Harvard, Vancouver, ISO, and other styles
More sources

Dissertations / Theses on the topic "Active aerodynamics"

1

Pesiridis, Apostolos. "Turbocharger turbine unsteady aerodynamics with active control." Thesis, Imperial College London, 2007. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.498148.

Full text
APA, Harvard, Vancouver, ISO, and other styles
2

Brzozowski, Daniel Paul. "Dynamic control of aerodynamic forces on a moving platform using active flow control." Diss., Georgia Institute of Technology, 2011. http://hdl.handle.net/1853/42930.

Full text
Abstract:
The unsteady interaction between trailing edge aerodynamic flow control and airfoil motion in pitch and plunge is investigated in wind tunnel experiments using a two degree-of-freedom traverse which enables application of time-dependent external torque and forces by servo motors. The global aerodynamic forces and moments are regulated by controlling vorticity generation and accumulation near the trailing edge of the airfoil using hybrid synthetic jet actuators. The dynamic coupling between the actuation and the time-dependent flow field is characterized using simultaneous force and particle image velocimetry (PIV) measurements that are taken phase-locked to the commanded actuation waveform. The effect of the unsteady motion on the model-embedded flow control is assessed in both trajectory tracking and disturbance rejection maneuvers. The time-varying aerodynamic lift and pitching moment are estimated from a PIV wake survey using a reduced order model based on classical unsteady aerodynamic theory. These measurements suggest that the entire flow over the airfoil readjusts within 2-3 convective time scales, which is about two orders of magnitude shorter than the characteristic time associated with the controlled maneuver of the wind tunnel model. This illustrates that flow-control actuation can be typically effected on time scales that are commensurate with the flow's convective time scale, and that the maneuver response is primarily limited by the inertia of the platform.
APA, Harvard, Vancouver, ISO, and other styles
3

Wu, Dong-Nan. "Active bounded-state vibration control for structural applications." Diss., Georgia Institute of Technology, 1995. http://hdl.handle.net/1853/12326.

Full text
APA, Harvard, Vancouver, ISO, and other styles
4

Chowdhury, Subhradeep. "An experimental investigation of active stall control in compression systems." Diss., Georgia Institute of Technology, 1995. http://hdl.handle.net/1853/12341.

Full text
APA, Harvard, Vancouver, ISO, and other styles
5

Griffin, Steven F. "Acoustic replication in smart structure using active structural/acoustic control." Diss., Georgia Institute of Technology, 1995. http://hdl.handle.net/1853/13085.

Full text
APA, Harvard, Vancouver, ISO, and other styles
6

Alan, Luton J. "Numerical simulations of subsonic aeroelastic behavior and flutter suppression by active control /." This resource online, 1991. http://scholar.lib.vt.edu/theses/available/etd-03172010-020348/.

Full text
APA, Harvard, Vancouver, ISO, and other styles
7

Williams, Nathan M. "Active flow control on a nonslender delta wing." Thesis, University of Bath, 2009. https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.501373.

Full text
Abstract:
The effects of active flow control by oscillatory blowing at the leading edge of a nonslender delta wing with a Λ=50° sweep angle have been investigated. Pressure measurements and Particle Image Velocimetry measurements were conducted on a half wing to investigate the formation of leading edge vortices for oscillatory blowing, compared to the stalled flow for the no blowing case. Stall has been delayed by up to 8, and significant increases in the upper surface suction force have been observed. Velocity measurements show that shear layer reattachment is promoted with forcing, and a vortex flow pattern develops. The time averaged location of the centre of the vortical region moves outboard with increased excitation. The near-surface flow pattern obtained from the PIV measurements shows reattachment in the forward part of the wing. There is no measurable jet-like axial flow in the vortex core, which seems to break down at or very near the apex. This highlights that unlike slender delta wings, vortex breakdown is not a limiting factor in the generation of lift for nonslender delta wings. Phase averaged measurements reveal the perturbation due to the pulsed blowing, its interaction with the shear layer and vortex, apparent displacement of the vortex core, and relaxation of the reattachment region. The flow in a phase averaged sense is highly three dimensional. Experiments indicate that unsteady blowing at Strouhal numbers in the region of St=0.5 to St=0.75, and in the region of St=1.25 to St=1.5 can be a highly effective. Reattached flow can develop from stalled flow after pulsing has been initiated with a time constant of tU/c=5 for unsteady blowing at St=0.75, and tU/c=7 for St=1.5. Experiments with excitation from finite span slots located in the forward half of the wing show that partial blowing can be more effective at low momentum coefficients. Force measurements of a full delta wing confirmed that the effectiveness of this method of flow control was not only confined to half delta wings.
APA, Harvard, Vancouver, ISO, and other styles
8

Stiborová, Dana. "Aktivní aerodynamické prvky osobních vozidel." Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2017. http://www.nusl.cz/ntk/nusl-318777.

Full text
Abstract:
In this diploma thesis active aerodynamic components are designed, specifically brake cooling duct and active automotive wing. Cooling duct prototype and also active regulation controlling electronics including the software were created. Road test was performed to measure the duct parameters. Construction design and the active regulation function of the automotive wing were created. The influence of the wing on aerodynamic characteristics of the car was determined.
APA, Harvard, Vancouver, ISO, and other styles
9

Krichene, Assaad. "Active identification and control of aerodynamic instabilities in axial and centrifugal compressors." Diss., Georgia Institute of Technology, 2001. http://hdl.handle.net/1853/12062.

Full text
APA, Harvard, Vancouver, ISO, and other styles
10

Kuchan, Abigail. "The integration of active flow control devices into composite wing flaps." Thesis, Georgia Institute of Technology, 2012. http://hdl.handle.net/1853/44758.

Full text
Abstract:
Delaying stall is always an attractive option in the aerospace industry. The major benefit of delaying stall is increased lift during takeoff and landings as well as during high angle of attack situations. Devices, such as fluidic oscillators, can be integrated into wing flaps to help delay the occurrence of stall by adding energized air to the airflow on the upper surface of the wing flap. The energized air from the oscillator allows the airflow to remain attached to the upper surface of the wing flap. The fluidic oscillator being integrated in this thesis is an active flow control device (AFC). One common method for integrating any device into a wing flap is to remove a section of the flap and mechanically secure the device. A current trend in the aerospace industry is the increased use of fiber-reinforced composites to replace traditional metal components on aircraft. The traditional methods of device integration cause additional complications when applied to composite components as compared to metal components. This thesis proposes an alternative method for integration of the AFC devices, which occurs before the fabrication of wing flaps is completed and they are attached to the aircraft wing. Seven design concepts are created to reduce the complications from using current methods of integration on composite wing flaps. The concepts are based on four design requirements: aerodynamics, manufacturing, maintenance, and structure. Four of the design concepts created are external designs, which place the AFC on the exterior surface of the wing flap in two types of grooved channels. The other three designs place the AFC inside the wing flap skin and are categorized as internal designs. In order for the air exiting the AFC to reach the upper surface of the wing flap, slots are created in the wing flap skin for the internal designs. Within each of the seven design concepts two design variants are created based on foam or ribbed core types. Prototypes were created for all of the external design AFC devices and the side inserted AFC and retaining pieces. Wing flap prototypes were created for the rounded groove straight AFC design, the semi-circular groove with straight AFC, and the side inserted AFC designs. The wing flaps were created using the VARTM process with a vertical layup for the external designs. The rounded groove and semi-circular groove prototypes each went through three generations of prototypes until an acceptable wing flap was created. The side inserted design utilized the lessons learned through each generation of the external design prototypes eliminating the need for multiple generations. The lessons learned through the prototyping process helped refine the designs and determine the ease of manufacturing to be used in the design evaluation. The evaluation of the designs is based on the four design requirements stated above. The assessment of the designs uses two levels of evaluation matrices to determine the most fitting design concept. As a result of the evaluation, all four of the external designs and one of the internal designs are eliminated. The two remaining internal designs' foam core and ribbed variants are compared to establish the final design selection. The vertically inserted AFC foam core design is the most fitting design concept for the integration of an AFC device into a composite wing flap.
APA, Harvard, Vancouver, ISO, and other styles
More sources

Books on the topic "Active aerodynamics"

1

Paduano, James D. Active control of rotating stall in axial compressors. Cambridge, Mass: Gas Turbine Laboratory, Massachusetts Institute of Technology, 1992.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
2

Nissim, E. Control surface spanwise placement in active flutter suppression systems. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
3

Haynes, Joel M. Active control of rotating stall in a three-stage axial compressor. Cambridge, Mass: Gas Turbine Laboratory, Massachusetts Institute of Technology, 1993.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
4

Nissim, E. Effect of control surface mass unbalance on the stability of a closed-loop active control system. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
5

Ravindran, S. S. Active control of flow separation over an airfoil. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
6

Ravindran, S. S. Active control of flow separation over an airfoil. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
7

Li, Feng-Chen. Turbulent drag reduction by surfactant additives. Hoboken, N.J: Wiley, 2011.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
8

Schwartz, Heather E. The science of a race car: Reactions in action. Mankato, Minn: Capstone Press, 2010.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
9

Schwartz, Heather E. The science of a race car: Reactions in action. Mankato, Minn: Capstone Press, 2010.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
10

S, Pototzky Anthony, and Langley Research Center, eds. Rolling maneuver load alleviation using active controls. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
More sources

Book chapters on the topic "Active aerodynamics"

1

Abo El lail, A. S., and A. S. Hassan. "Active Suppression of Compressor Flow Instability." In Unsteady Aerodynamics and Aeroelasticity of Turbomachines, 495–509. Dordrecht: Springer Netherlands, 1998. http://dx.doi.org/10.1007/978-94-011-5040-8_32.

Full text
APA, Harvard, Vancouver, ISO, and other styles
2

Stalnov, Oksana. "Closed-loop Active Flow Control for UAVs." In Advanced UAV Aerodynamics, Flight Stability and Control, 447–64. Chichester, UK: John Wiley & Sons, Ltd, 2017. http://dx.doi.org/10.1002/9781118928691.ch13.

Full text
APA, Harvard, Vancouver, ISO, and other styles
3

De Cupis, Davide, Henrique de Carvalho Pinheiro, Alessandro Ferraris, Andrea Giancarlo Airale, and Massimiliana Carello. "Active Aerodynamics Design Methodology for Vehicle Dynamics Enhancement." In Mechanisms and Machine Science, 777–85. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-55807-9_86.

Full text
APA, Harvard, Vancouver, ISO, and other styles
4

Marqués, Pascual. "Active Blade Twist in Rotary UAVs using Smart Actuation." In Advanced UAV Aerodynamics, Flight Stability and Control, 399–419. Chichester, UK: John Wiley & Sons, Ltd, 2017. http://dx.doi.org/10.1002/9781118928691.ch11.

Full text
APA, Harvard, Vancouver, ISO, and other styles
5

Lombardi, Giovanni, Marco Maganzi, and Elena Pasqualetto. "Active aerodynamics to increase the features of a motorcycle." In Proceedings, 135–49. Wiesbaden: Springer Fachmedien Wiesbaden, 2020. http://dx.doi.org/10.1007/978-3-658-29943-9_14.

Full text
APA, Harvard, Vancouver, ISO, and other styles
6

Lawless, Patrick B., and Sanford Fleeter. "Active Control of Centrifugal Compressor Rotating Stall." In Unsteady Aerodynamics, Aeroacoustics, and Aeroelasticity of Turbomachines and Propellers, 397–414. New York, NY: Springer New York, 1993. http://dx.doi.org/10.1007/978-1-4613-9341-2_20.

Full text
APA, Harvard, Vancouver, ISO, and other styles
7

El-Alti, Mohammad, Valery Chernoray, Per Kjellgren, Linus Hjelm, and Lars Davidson. "Computations and Full-Scale Tests of Active Flow Control Applied on a VOLVO Truck-Trailer." In The Aerodynamics of Heavy Vehicles III, 253–67. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-20122-1_16.

Full text
APA, Harvard, Vancouver, ISO, and other styles
8

Bruneau, Charles-Henri, Emmanuel Creusé, Delphine Depeyras, Patrick Gilliéron, and Iraj Mortazavi. "Analysis of the Active and Passive Drag Reduction Strategies Behind a Square Back Ground Vehicle." In The Aerodynamics of Heavy Vehicles III, 363–76. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-20122-1_23.

Full text
APA, Harvard, Vancouver, ISO, and other styles
9

Seifert, A., O. Stalnov, D. Sperber, G. Arwatz, V. Palei, S. David, I. Dayan, and I. Fono. "Large Trucks Drag Reduction using Active Flow Control." In The Aerodynamics of Heavy Vehicles II: Trucks, Buses, and Trains, 115–33. Berlin, Heidelberg: Springer Berlin Heidelberg, 2009. http://dx.doi.org/10.1007/978-3-540-85070-0_10.

Full text
APA, Harvard, Vancouver, ISO, and other styles
10

Iaccarino, G., B. de Maio, R. Verzicco, and B. Khalighi. "RANS Simulations of Passive and Active Drag Reduction Devices for a Road Vehicle." In The Aerodynamics of Heavy Vehicles: Trucks, Buses, and Trains, 267–75. Berlin, Heidelberg: Springer Berlin Heidelberg, 2004. http://dx.doi.org/10.1007/978-3-540-44419-0_25.

Full text
APA, Harvard, Vancouver, ISO, and other styles

Conference papers on the topic "Active aerodynamics"

1

de Carvalho Pinheiro, Henrique, Francesco Russo, Lorenzo Sisca, Alessandro Messana, Davide De Cupis, Alessandro Ferraris, Andrea Giancarlo Airale, and Massimiliana Carello. "Advanced Vehicle Dynamics Through Active Aerodynamics and Active Body Control." In ASME 2020 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. American Society of Mechanical Engineers, 2020. http://dx.doi.org/10.1115/detc2020-22290.

Full text
Abstract:
Abstract In this paper, the development procedure of an innovative control algorithm is shown, with the aim of improving handling performance of a high-end sport vehicle by actively controlling aerodynamic forces acting on the vehicle itself. The proposed control algorithm operates indirectly by modifying ride-heights of the vehicle through an active suspensions system. The vehicle dynamics analysis is conducted in parallel to the aerodynamics analysis performed in a concurrent engineering operation. The software used for control algorithms development is VI-CarRealTime, in co-simulation with Matlab-Simulink, with an extended use of the MaxPerformance package. Specific tracks have been implemented ad hoc to highlight the effects of the control systems operation in development phase. To better explore the potential of the technique, a fuzzy logic system was developed.
APA, Harvard, Vancouver, ISO, and other styles
2

Vaccaro, John, Michael Amitay, and Joseph Vasile. "Active Control of Inlet Ducts." In 26th AIAA Applied Aerodynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2008. http://dx.doi.org/10.2514/6.2008-6402.

Full text
APA, Harvard, Vancouver, ISO, and other styles
3

Roget, Beatrice. "Simulation of Active Twist and Active Flap Control on a Model-Scale Helicopter Rotor." In 24th AIAA Applied Aerodynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/6.2006-3473.

Full text
APA, Harvard, Vancouver, ISO, and other styles
4

Meyer, Michael, Wolfgang Machunze, and Matthias Bauer. "Towards the Industrial Application of Active Flow Control in Civil Aircraft - An Active Highlift Flap." In 32nd AIAA Applied Aerodynamics Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2014. http://dx.doi.org/10.2514/6.2014-2401.

Full text
APA, Harvard, Vancouver, ISO, and other styles
5

Sobieczky, Helmut, and Wolfgang Giessler. "Active flow control based on transonic design concepts." In 17th Applied Aerodynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1999. http://dx.doi.org/10.2514/6.1999-3127.

Full text
APA, Harvard, Vancouver, ISO, and other styles
6

Kerho, Michael, Joseph Heid, Brian Kramer, and Terry Ng. "Active drag reduction using selective low rate suction." In 18th Applied Aerodynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/6.2000-4018.

Full text
APA, Harvard, Vancouver, ISO, and other styles
7

Caruana, Daniel, André Mignosi, Michel Correge, and Alain Le Pourhiet. "Buffeting Active Control in Transonic Flow." In 21st AIAA Applied Aerodynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2003. http://dx.doi.org/10.2514/6.2003-3667.

Full text
APA, Harvard, Vancouver, ISO, and other styles
8

Kauth, Felix, Joerg R. Seume, Rolf Radespiel, Richard Semaan, Daniela G. François, Yosef El Sayed M., Christian Behr, et al. "Progress in Efficient Active High-Lift." In 35th AIAA Applied Aerodynamics Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2017. http://dx.doi.org/10.2514/6.2017-3559.

Full text
APA, Harvard, Vancouver, ISO, and other styles
9

Dunne, James, Dale Pitt, Kevin Kilian, and Donald Sofge. "Recent advances in active damage interrogation." In 19th AIAA Applied Aerodynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2001. http://dx.doi.org/10.2514/6.2001-1442.

Full text
APA, Harvard, Vancouver, ISO, and other styles
10

Othmer, Carsten, Trent W. Lukaczyk, Paul Constantine, and Juan J. Alonso. "On Active Subspaces in Car Aerodynamics." In 17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2016. http://dx.doi.org/10.2514/6.2016-4294.

Full text
APA, Harvard, Vancouver, ISO, and other styles

Reports on the topic "Active aerodynamics"

1

Griffin, D. A., and T. J. McCoy. COE Reductions through Active Aerodynamic Control of Rotor Aerodynamics and Geometry. Office of Scientific and Technical Information (OSTI), December 2008. http://dx.doi.org/10.2172/945953.

Full text
APA, Harvard, Vancouver, ISO, and other styles
You might also be interested in the extended bibliographies on the topic 'Active aerodynamics' for particular source types:
Journal articles Dissertations / Theses Books
We offer discounts on all premium plans for authors whose works are included in thematic literature selections. Contact us to get a unique promo code!

To the bibliography