Abstract
The design integration of a supersonic combustion ramjet engine (SCRAMJET) with an airframe remains a critical task for guarantying a successful mission of trans atmospheric or hypersonic cruise vehicles. For this purpose, the operational efficiency has to be established by the effective specific impulse and the thrust to weight ratio of the accelerating vehicle. In order to analyze the foregoing problems, a design methodology based on Evolutionary Algorithms (EAs) and Game Strategies (GS) is developed. In this study, Evolutionary Algorithms (EAs) are used to solve MDO problems. The proposed methodology is tested and its performances and quality design evaluated for optimizing a 2-D air-breathing hypersonic vehicle shape at cruise flight conditions: Euler flow, Mach number = 8; angle of attack = 0°; flight altitude = 30 km, involving aerodynamics, thermodynamics and propulsion disciplines. The set up of an operational flight corridor requires a compromise among air-breathing engine performance, vehicle aerodynamic performance, and structural thermal load limit resulting from aero-heating. For this purpose, the operational efficiency is established by the effective specific impulse and thrust to weight ratio of the accelerating vehicle. In order to analyze the foregoing problems, a methodology is developed, which permits a quick performance evaluation of an idealized, integrated SCRAMJET vehicle for preliminary design analysis. A Pareto-EAs methodology is used to find design and off design solutions of an integrated vehicle consisting of the fore body inlet, the supersonic flow combustor and the after body expansion nozzle. From preliminary numerical experiments on a generic test case 2-D air breathing vehicle and analysis of results, the Pareto-EAs numerical approach is a promising methodology with game coalition for its use in industrial aeronautical design and well suited for its implementation on HPCs for increasing its efficiency.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Study of an Air-Breathing Engine for Hypersonic Flight (Figs. 9–10) (PDF). Universitat Politecnica de Catalunya. Retrieved 3 June 2015
Harsha, P.T., Keel, L.C., Castrogiovanni, A., Sherrill, R.T.: X-43A vehicle design and manufacture. AIAA 2005–3334
Heiser, W.H., Pratt, D.T., Daley, D.H., Mehta, U.B.: Hypersonic Airbreathing Propulsion. American Institute of Aeronautics and Astronautics, Washington, D.C (1994)
Roudakov, A., Semenov, V., Hicks, J.: Recent flight test results of the joint CIAMNASA Mach 6.5 Scramjet Flight Program. NASA/TP-1998-206548
Waltrup, P.J., White, M.E., Zarlingo, F., Gravlin, E.S.: History of Ramjet and Scramjet Propulsion Development for U.S. Navy Missiles, 50 years Milton S. Eisenhower R&T Center (1997)
Pareto, V.: Cours d’Economie Politique. Rouge, Lausanne, Switzerland (1896)
Deb, K.: Multi-Objective Optimization Using Evolutionary Algorithms. Wiley (2003)
Periaux, J., Gonzalez, F., Lee, D.C.: Evolutionary Optimization and Game Strategies for Advanced Design: Applications to Aeronautics, Control and Automation. Science and Engineering Series, vol. 75. Springer (2015)
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2019 Springer International Publishing AG
About this chapter
Cite this chapter
Wu, P., Tang, Z., Periaux, J. (2019). Multi-disciplinary Design Optimization of Air-Breathing Hypersonic Vehicle Using Pareto Games and Evolutionary Algorithms. In: Minisci, E., Vasile, M., Periaux, J., Gauger, N., Giannakoglou, K., Quagliarella, D. (eds) Advances in Evolutionary and Deterministic Methods for Design, Optimization and Control in Engineering and Sciences. Computational Methods in Applied Sciences, vol 48. Springer, Cham. https://doi.org/10.1007/978-3-319-89988-6_19
Download citation
DOI: https://doi.org/10.1007/978-3-319-89988-6_19
Published:
Publisher Name: Springer, Cham
Print ISBN: 978-3-319-89986-2
Online ISBN: 978-3-319-89988-6
eBook Packages: EngineeringEngineering (R0)