Hypersonic Flow
Vehicle Design
  1. Anderson, John D., Jr. Hypersonic and High Temperature Gas Dynamics. NY: McGraw-Hill, 1989.
  2. Anderson, John D., Jr. Modern Compressible Flow: With Historical Perspective. NY: McGraw-Hill, 1990, pp. 472-509.
  3. Anderson, John D., Jr. Introduction to Flight, 4th ed. Boston: McGraw-Hill, 2000, pp. 622-626 and 681-707.
  4. Bowcutt, Kevin G., Anderson, John D., Jr., and Capriotti, Diego. Viscous Optimized Hypersonic Waveriders, AIAA Paper 87-0272, 1987.
  5. Campbell, John M. and Pape, Garry R. North American XB-70 Valkyrie: A Photo Chronicle. Atglen, PA: Schiffer Military History, 1996.
  6. Capriotti, Diego, personal communication.
  7. Cockrell, Charles E. Interpretation of Waverider Performance Data Using Computational Fluid Dynamics, AIAA Paper 93-2921, 1993.
  8. Cockrell, Charles E. and Huebner, Lawrence D. Aerodynamic Characteristics of Two Waverider-Derived Hypersonic Cruise Configurations, NASA TP-3559, 1996.
  9. Cockrell, Charles E., Huebner, Lawrence D, and Finley, Dennis B. Aerodynamic Performance and Flow-Field Characteristics of Two Waverider-Derived Hypersonic Cruise Configurations, AIAA Paper 95-0736, 1995.
  10. Corda, Stephen and Anderson, John D., Jr. Viscous Optimized Waveriders Designed from Axisymmetric Flow Fields, AIAA Paper 88-0369, 1988.
  11. Douglass, Steve. B-3 and Beyond, Popular Science, vol. 256, no. 2, February 2000, pp. 46-50.
  12. Dryden Research Aircraft Photo Gallery,
  13. Eggers, A. J., Jr. and Syvertson, Clarence A. Aircraft Configurations Developing High Lift-Drag Ratios at High Supersonic Speeds, NACA RM-A55L05, 1956.
  14. Federation of American Scientists mystery aircraft site,
  15. Hahne, David E. Evaluation of the Low-Speed Stability and Control Characteristics of a Mach 5.5 Waverider Concept, NASA TM-4756, 1997.
  16. Hallion, Richard P., ed. The Hypersonic Revolution: Case Studies in the History of Hypersonic Technology, vol. 2: From Scramjet to the National Aero-Space Plane, 1964-1986. Bolling AFB: Air Force History and Museums Program, 1998.
  17. Hill, Philip G. and Peterson, Carl R. Mechanics and Thermodynamics of Propulsion. Reading, MA: Addison-Wesley Publishing, 1992, pp. 538-540.
  18. Miele, Angelo. Theory of Optimum Aerodynamic Shapes; External Problems in the Aerodynamics of Supersonic, Hypersonic, and Free-Molecular Flows. NY: Academic Press, 1965.
  19. Miller, Rolf W., Argrow, Brian M., Center, Kenneth B., Brauckmann, Gregory J., and Rhode, Matthew N. Experimental Verification of the Osculating Cones Method for Two Waverider Forebodies at Mach 4 and 6, AIAA Paper 98-0682, 1998.
  20. NASA Hyper-X fact sheet,
    (No longer available)
  21. Oates, Gordon C. Aerothermodynamics of Gas Turbine and Rocket Propulsion. Washington DC: American Institute of Aeronautics and Astronautics, 1988, pp. 140-158.
  22. Pegg, Robert J., Cockrell, Charles E., and Hahne, David E. Low-Speed Wind Tunnel Tests of Two Waverider Configuration Models, AIAA Paper 95-6093, 1995.
  23. Rees, Ed. The Manned Missile: The Story of the B-70. NY: Duell, Sloan, and Pearce, 1960.
  24. Sabean, John W. and Lewis, Mark J. Performance of a Power Law Star Body, AIAA Paper 98-1617, 1998.
  25. Schweikart, Larry. The Hypersonic Revolution: Case Studies in the History of Hypersonic Technology, vol. 3: The Quest for the Orbital Jet, the National Aero-Space Plane Program, 1983-1995. Bolling AFB: Air Force History and Museums Program, 1998.
  26. Siuru, Bill and Busick, John D. Future Flight: The Next Generation of Aircraft Technology, 2nd ed. Blue Ridge Summit, PA: TAB Books, 1994, pp. 60-65.
  27. STAAR Research -- An Historical Overview of Waverider Evolution,
  28. Starkey, Ryan P. and Lewis, Mark J. A Simple Analytical Model for Parametric Studies of Hypersonic Waveriders, AIAA Paper 98-1616, 1998.
  29. Tirpak, John A. Mission to Mach 5, Air Force Magazine, vol. 82, no. 1, January 1999.

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