Affiliation:
1. Nanjing University of Aeronautics and Astronautics, Nanjing 210016, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Reference16 articles.
1. Possibilities for Improved Supersonic Inlet Performance
2. MahoneyJ. J., Inlets for Supersonic Missiles, AIAA Education Series, AIAA, Washington, D.C., 1990, pp. 55–66.
3. KantrowitzA.DonaldsonC. “Preliminary Investigation of Supersonic Diffuser,” NACA Rept. WRL-713, 1945.
4. JohnsonH. J.MontoyaE. J. “Local Flow Measurements at the Inlet Spike Tip of a Mach 3 Supersonic Cruise Airplane,” NASA TN-D-6987, May 1973.
Cited by
11 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献