Analysis of experimental results on a Mach 14 waverider with blunt leading edges
Author:
Affiliation:
1. U.S. Navy, Naval Surface Warfare Center, Silver Spring, MD
2. Maryland, Univ., College Park
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-812
Reference22 articles.
1. Bowcutt, K. G. and Anderson, J. D., Jr. "ViscousOptimized Waveriders,"AIAA Paper 87-0272,Jan. 1987.
2. Burnett,D.andLewis,M. "ARe-Evaluationof the Waverider Design Process," AIAA Paper 93-0404,Jan.1993.
3. Tincher, D. J., and Burnett, D. "A Hypersonic Waverider Flight Test Vehicle: The Next Logical Step,"AIAAPaper 92-0308,Jan.1992.
4. Berry, C., Kammeyer, M., Larach, E., and Burnett, D. "Experiences in Fabrication of a Waverider Model for Wind Tunnel Testing," AIAA Paper 93-0510,Jan.1993.
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