The effect of Reynolds number on boattail drag
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, Va.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1975-63
Cited by 5 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
1. Reynolds number and model scale effects on F-16 nozzle-afterbody forces;17th Joint Propulsion Conference;1981-07-27
2. Engine/Aircraft Afterbody Interactions: Recommended Testing Techniques Based on YF-17 Experience;Journal of Aircraft;1980-11
3. Effects of Reynolds number and other parameters on the throttle-dependent, nozzle/afterbody drag of an 0.11 scale single-engine aircraft model;15th Joint Propulsion Conference;1979-06-18
4. Numerical solution of axisymmetric boattail flow fields with plume simulators;15th Aerospace Sciences Meeting;1977-01-24
5. Effect of Reynolds number on the nozzle afterbody performance of theAGARD nozzle afterbody and the B-1 0.06-scale model at transonic Mach numbers;11th Propulsion Conference;1975-08-16
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