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Concepts of Hypersonic Aircraft

  • P. Perrier

Abstract

Obviously, all concept of any aircraft is a compromise between conflicting requirements. Performance improvements generally induce direct cost.

Keywords

Mach Number Delta Wing Hypersonic Vehicle Sweep Angle Flight Control System 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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References

  1. (1).
    Dassault Aviation report 1.11.34 Winglet-vertical tail choice for HermesGoogle Scholar
  2. (2).
    Allen H. Whitehead, “Nasp Aerodynamics”. AIAA First National Aerospace Plane Conference, Paper n° 89–5013, Dayton, OH, July 20–21 1989.Google Scholar
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    David H. Campbell, “F-12 series aircraft propulsion system performance and development”, AIAA 5th Aircraft Design, Flight Test and Operations Meeting, Paper n° 73–821, St Louis, Missouri, August 6–8, 1973.Google Scholar
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    M. Rigault, “A Methodology for the Concept Definition of Advanced Space Transportation Systems”, conference EAC 89, Bonn-Bad Godesderg, 23 may 1989.Google Scholar
  5. (5).
    Wolfgang Schmidt “Aerodynamics of High Speed Air Intakes”, Status Report on FDP— WG13 Agard Pep 75th Symposium Madrid — May 1990.Google Scholar
  6. (6).
    M. Mallet, J. Periaux, P. Perrier, B. Stoufflet, “Flow Modelization and Computational Methodologies for the Aerothermal Design of Hypersonic Vehicles: Application to the European Hermes”. AIAA Thermophysics, Plasma dynamics and lasers conference, Paper n° 88–2628, San Antonio, Texas, June 27–29, 1988.Google Scholar
  7. (7).
    M. Mallet, J. Periaux and G. Roge, “Development of Finite Element Methods for Compressible Navier Stokes Flow Simulations in Aerospace Design”. AIAA Aerospace Sciences Meeting, Paper n° 90–0403, Reno, Nevada, January 8–11, 1990.Google Scholar

Copyright information

© Springer Science+Business Media New York 1992

Authors and Affiliations

  • P. Perrier
    • 1
  1. 1.Dassault AviationFrance

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