Numerical solution of axisymmetric boattail flow fields with plume simulators
Author:
Affiliation:
1. NASA, Langley Research Center, High-Speed AerodynamicsDiv., Hampton, Va.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1977-224
Reference19 articles.
1. Z y n a m, I, E., and Abryounis, 51. K. "Experimental and Thcorcticnl Study of Flow Fields Surrounding Bmttnil Nozzles at Suhsonic Specds," AIM Pnptx No. 76-675, July 3976.
2. The effect of Reynolds number on boattail drag
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