Nacelle Integration Study on a Mach-2.2 Supersonic Cruise Aircraft
Author:
Affiliation:
1. McDonnell Douglas Corporation, Long Beach, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.58895
Reference11 articles.
1. AST - A Fifth Engine For Environmental Consideration
2. Advanced Supersonic Transport
3. 5Gentry, A.E., Smyth, D.N., and Oliver, W.R. "The Mark IV Supersonic-Hypersonic Arbitrary-Body Program," AFFDL-TR-73-159,1973.
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2. Shape Optimizing Nacelle near Flat-Plate Wing Using Multiblock Sensitivity Analysis;Journal of Aircraft;1998-01
3. Inlet Design Studies for a Mach 2.2 Advanced Supersonic Cruise Vehicle;Journal of Aircraft;1982-07
4. Advanced supersonic transport propulsion and configuration technology improvements;17th Joint Propulsion Conference;1981-07-27
5. Inlet design studies for a Mach 2.2 advanced supersonic cruise vehicle;Aircraft Systems and Technology Meeting;1979-08-17
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