The numerical computation of the transonic flow over afterbodies including the effect of jet-plume and viscous interactions
Author:
Affiliation:
1. Grumman Aerospace Corp., Bethpage, N.Y.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1975-62
Cited by 7 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. Navier-Stokes solutions for an axisymmetric nozzle;17th Joint Propulsion Conference;1981-07-27
2. Overlaid Viscous/Anviscid Model for the Prediction of Near-Field Jet Entrainment;AIAA Journal;1979-09
3. Boundary layer flows on transonic projectiles;12th Fluid and Plasma Dynamics Conference;1979-07-23
4. Evaluation of methods for prediction of propulsion system drag;15th Joint Propulsion Conference;1979-06-18
5. Numerical investigation of the external flow over the after-body and the flow within the nozzle for different jet regimes;Fluid Dynamics;1979
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