Literatura científica selecionada sobre o tema "Aero-Propulsive"
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Artigos de revistas sobre o assunto "Aero-Propulsive"
STEPAN, Anca, Georges GHAZI e Ruxandra Mihaela BOTEZ. "Development of an Adaptive Aero-Propulsive Performance Model in Cruise Flight – Application to the Cessna Citation X". INCAS BULLETIN 14, n.º 4 (2 de dezembro de 2022): 167–81. http://dx.doi.org/10.13111/2066-8201.2022.14.4.14.
Texto completo da fonteZhao, Wenyuan, Yanlai Zhang, Peng Tang e Jianghao Wu. "The Impact of Distributed Propulsion on the Aerodynamic Characteristics of a Blended-Wing-Body Aircraft". Aerospace 9, n.º 11 (10 de novembro de 2022): 704. http://dx.doi.org/10.3390/aerospace9110704.
Texto completo da fonteLuo, Shaojun, Tian Zi Eng, Zhili Tang, Qianrong Ma, Jinyou Su e Gabriel Bugeda. "Multidisciplinary Optimization of Aircraft Aerodynamics for Distributed Propulsion Configurations". Applied Sciences 14, n.º 17 (3 de setembro de 2024): 7781. http://dx.doi.org/10.3390/app14177781.
Texto completo da fonteSeitz, Arne, Anaïs Luisa Habermann, Fabian Peter, Florian Troeltsch, Alejandro Castillo Pardo, Biagio Della Corte, Martijn van Sluis et al. "Proof of Concept Study for Fuselage Boundary Layer Ingesting Propulsion". Aerospace 8, n.º 1 (13 de janeiro de 2021): 16. http://dx.doi.org/10.3390/aerospace8010016.
Texto completo da fonteBaklacioglu, T., e M. Cavcar. "Aero-propulsive modelling for climb and descent trajectory prediction of transport aircraft using genetic algorithms". Aeronautical Journal 118, n.º 1199 (janeiro de 2014): 65–79. http://dx.doi.org/10.1017/s0001924000008939.
Texto completo da fonteSwain, Prafulla Kumar, Ashok K. Barik, Siva Prasad Dora e Rajeswara Resapu. "The propulsion of tandem flapping foil following fishtailed flapping trajectory". Physics of Fluids 34, n.º 12 (dezembro de 2022): 123609. http://dx.doi.org/10.1063/5.0128223.
Texto completo da fonteYin, F., e A. Gangoli Rao. "Performance analysis of an aero engine with inter-stage turbine burner". Aeronautical Journal 121, n.º 1245 (4 de setembro de 2017): 1605–26. http://dx.doi.org/10.1017/aer.2017.93.
Texto completo da fonteCorcione, Salvatore, Vincenzo Cusati, Danilo Ciliberti e Fabrizio Nicolosi. "Experimental Assessment of Aero-Propulsive Effects on a Large Turboprop Aircraft with Rear-Engine Installation". Aerospace 10, n.º 1 (15 de janeiro de 2023): 85. http://dx.doi.org/10.3390/aerospace10010085.
Texto completo da fonteMinucci, Marco A. S., e Leik N. Myrabo. "Phase distortion in a propulsive laser beam due to aero-optical phenomena". Journal of Propulsion and Power 6, n.º 4 (julho de 1990): 416–25. http://dx.doi.org/10.2514/3.25452.
Texto completo da fontePerry, Aaron T., Phillip J. Ansell e Michael F. Kerho. "Aero-Propulsive and Propulsor Cross-Coupling Effects on a Distributed Propulsion System". Journal of Aircraft 55, n.º 6 (novembro de 2018): 2414–26. http://dx.doi.org/10.2514/1.c034861.
Texto completo da fonteTeses / dissertações sobre o assunto "Aero-Propulsive"
Altamirano, George V. "Investigation of Longitudinal Aero-Propulsive Interactions of a Small Quadrotor Unmanned Aircraft System". The Ohio State University, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=osu1607075603449697.
Texto completo da fonteDosne, Cyril. "Development and implementation of adjoint formulation of explicit body-force models for aero-propulsive optimizations". Electronic Thesis or Diss., Institut polytechnique de Paris, 2024. http://www.theses.fr/2024IPPAX026.
Texto completo da fonteIn civil aviation, the increasing exploration of innovative engine systems – such as ultra-high bypass ratio turbofan or open-rotor – and breakthrough engine-integration architectures – such as distributed propulsion or boundary-layer ingestion – require a coupled modeling of the aerodynamic and propulsion subsystems from the earliest design stages. Body-force models have proven capable of faithfully reproducing most of the coupling phenomena, such as the engine response to inlet flow distortions, at reduced computational cost. However, they lack an adjoint formulation to be efficiently used in gradient-based optimizations. The present PhD thesis focuses on the development of an adjoint approach for explicit body-force models. First, aero-propulsive optimizations of an academic distributed propulsion configuration are conducted using a lumped body-force model. Despite the simplicity of this model (of interest for conceptual design studies), 10.5% decrease in power consumption is achieved. Then the potential of this new methodology is investigated for the preliminary optimization of compressor stages, at first under clean inflow conditions. The Hall body-force model is considered for such purpose. The comparison of the blade shape gradients computed by the adjoint body-force with high-fidelity ones, obtained from blade-resolved computations, shows very good prediction for the rotor. This is observed over a large portion of the compressor characteristic, especially between near-design and surge operating conditions, while accuracy is reduced near the blockage. On the contrary, for stator shape gradients, only flow misalignment effects can be captured. At design conditions, the improvement of the compressor efficiency obtained by the adjoint body-force optimization has been confirmed through high-fidelity simulations. Optimization under radial inlet distortion are then investigated. Once again, the adjoint body-force approach is found capable of enhancing the compressor performances, by adapting its geometry to the off-design inflow conditions. According to high-fidelity analysis of the body-force optimized blade geometry, an increase in compressor isentropic efficiency between 1.16 and 1.47% is achieved, given the formulation of the optimization problem. Finally, an optimization of the compressor under full-annulus inlet distortion is conducted leading to very promising results, which are consistent with those found in the literature using advanced simulations
Arntz, Aurélien. "Civil aircraft aero-thermo-propulsive performance assessment by an exergy analysis of high-fidelity CFD-RANS flow solutions". Thesis, Lille 1, 2014. http://www.theses.fr/2014LIL10110/document.
Texto completo da fonteThe tools and methodologies currently used for the design of commercial aircraft have been initiated decades ago and are based on simplifying assumptions that become excessively ambiguous for highly-integrated propulsion devices for which traditional drag/thrust bookkeepings become inapplicable. Likewise, the growing complexity of civil aircraft requires a more global performance assessment which could take into account thermal management. As a consequence, a new exergy-based formulation is derived for the assessment of the aerothermopropulsive performance of civil aircraft. The output of the derivation process is an exergy balance between the exergy supplied by a propulsion system or by heat transfer, the mechanical equilibrium of the aircraft, and the exergy outflow and destruction within the control volume. The theoretical formulation is subsequently numerically implemented in a Fortran code named ffx for the post-processing of CFD-RANS flow solutions. Unpowered airframe configurations are examined with grid refinement studies and a turbulence model sensitivity analysis. The code is thereby validated against well-tried methods of drag prediction or wind-tunnel testings when available. Finally, the investigation of powered configurations demonstrates the ability of the approach for the performance assessment of configurations with aerothermopropulsive interactions
"Modeling, Analysis, and Control of a Hypersonic Vehicle With Significant Aero-Thermo-Elastic-Propulsion Interactions, and Propulsive Uncertainty". Master's thesis, 2010. http://hdl.handle.net/2286/R.I.8592.
Texto completo da fonteDissertation/Thesis
M.S. Electrical Engineering 2010
Capítulos de livros sobre o assunto "Aero-Propulsive"
Wervaecke, Christelle, Ilias Petropoulos e Didier Bailly. "Assessment of Exergy Analysis of CFD Simulations for the Evaluation of Aero-Thermo-Propulsive Performance of Aerial Vehicles". In Computational Methods in Applied Sciences, 261–75. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-57422-2_17.
Texto completo da fonteTrabalhos de conferências sobre o assunto "Aero-Propulsive"
Geuther, Steven, Benjamin Simmons e Kasey Ackerman. "Overview of the Subscale RAVEN Flight Controls and Modeling Testbed". In Vertical Flight Society 80th Annual Forum & Technology Display, 1–12. The Vertical Flight Society, 2024. http://dx.doi.org/10.4050/f-0080-2024-1185.
Texto completo da fonteTOWNEND, L., E. BROADBENT, J. CLARKE, R. EAST, T. NONWEILER, G. PAGAN, E. PARKER e J. PIKE. "Aero-propulsive effects on configuration shaping". In 3rd International Aerospace Planes Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-5064.
Texto completo da fonteAhuja, Vivek, Imon Chakraborty e Roy J. Hartfield. "Aero-Propulsive Analysis for Contemporary Conceptual Design". In AIAA Aviation 2019 Forum. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2019. http://dx.doi.org/10.2514/6.2019-3019.
Texto completo da fontede Vries, Reynard, Maurice Hoogreef e Roelof Vos. "Aero-Propulsive Efficiency Requirements for Turboelectric Transport Aircraft". In AIAA Scitech 2020 Forum. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2020. http://dx.doi.org/10.2514/6.2020-0502.
Texto completo da fonteAfricawala, Jalendu, e Aleksandar Joksimovic. "Panel Method for Aero-Propulsive Design Space Exploration". In AIAA SCITECH 2024 Forum. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2024. http://dx.doi.org/10.2514/6.2024-0240.
Texto completo da fonteKerho, Mike F. "Aero-Propulsive Coupling of an Embedded, Distributed Propulsion System". In 33rd AIAA Applied Aerodynamics Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2015. http://dx.doi.org/10.2514/6.2015-3162.
Texto completo da fonteHosangadi, A., P. Cavallo, S. Arunajatesan, R. Ungewitter e R. Lee. "Aero-propulsive jet interaction simulations using hybrid unstructured meshes". In 35th Joint Propulsion Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1999. http://dx.doi.org/10.2514/6.1999-2119.
Texto completo da fonteGORADIA, SURESH, ABEL TORRES, SHARON STACK e JOEL EVERHART. "Engineering method for aero-propulsive characteristics at hypersonicMach numbers". In 3rd International Aerospace Planes Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-5061.
Texto completo da fonteSagliano, Marco, Ping Lu, Breanna Johnson, David Seelbinder e Stephan Theil. "Six-Degrees-of-Freedom Aero-Propulsive Entry Trajectory Optimization". In AIAA SCITECH 2024 Forum. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2024. http://dx.doi.org/10.2514/6.2024-1171.
Texto completo da fonteSimmons, Benjamin M., James L. Gresham e Craig A. Woolsey. "Aero-Propulsive Modeling for Propeller Aircraft Using Flight Data". In AIAA SCITECH 2022 Forum. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2022. http://dx.doi.org/10.2514/6.2022-2171.
Texto completo da fonte