Conceptual design of a Mach 10, global reach reconnaissance aircraft
Author:
Affiliation:
1. McDonnell Douglas Aerospace, Saint Louis, MO
2. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-2894
Reference12 articles.
1. O'Neill, M. K. and Lewis, M.J., Optimized Scramjet Integration onaWavcrider,/.of Aircraft, 29, 1114(1992).
2. Haney,J. W.andBeaulieu,W.D.,Waverider Inlet Integration Issues,32nd AIAA Aerospace Sciences Meeting, Rcno, NV,January 1994,AIAA Paper94-0383.
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