Preliminary flight and wind tunnel comparisons of the inlet/airframe interaction of the F-15 airplane
Author:
Affiliation:
1. NASA, Flight Research Center, Edwards, Calif.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1979-102
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1. Numerical Study on Variation in Drag Difference by Adding Annular Plug into Flow-Through Nacelle with Integrated Configuration;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN;2024
2. Capture Area Ratio and Drag Difference between Wind Tunnel and Flight Tests;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2022
3. Experience with flight test trajectory guidance;Journal of Guidance, Control, and Dynamics;1983-09
4. Review of Flight-to-Wind-Tunnel Drag Correlation Edwin;Journal of Aircraft;1982-10
5. Recent propulsion system flight tests at the NASA Dryden Flight Research Center;1st Flight Test Conference;1981-08-17
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