An analytical method to compute viscous-inviscid transonic flow on axisymmetric afterbodies including jet effects and boattail bleed in separated regions
Author:
Affiliation:
1. USAF, Flight Dynamics Laboratory, Wright-Patterson AFB, Ohio
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1975-1293
Reference18 articles.
Cited by 3 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. Mass Injection and Jet Flow Simulation Effects on Transonic Afterbody Drag;Journal of Aircraft;1979-07
2. Mass injection and jet flow simulation effects on transonic afterbody drag;11th Fluid and PlasmaDynamics Conference;1978-07-10
3. Experimental and theoretical study of flow fields surrounding boattail nozzles at subsonic speeds;12th Propulsion Conference;1976-07-26
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