Computation of a supersonic flow past an axisymmetric nozzle boattail with jet exhaust
Author:
Affiliation:
1. Dayton, University, Dayton, Ohio
2. USAF, Flight Dynamics Laboratory, Wright-Patterson AFB, Ohio
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1978-993
Reference25 articles.
1. HOISt, T. L. "Numerical Solution of Axisymmetric Boattail Fields with Plume Simulators,'' AIAA Paper 74-224, January 1977.
2. Numerical Simulation of Realistic High-speed Inlets Using the Navier-Stokes Equations
3. Mikhail, A. G. "Computation of a Supersonic Flow Past an Axisymrnetric Nozzle Boattail with Jet Exhaust," to be published as an AFFDL Technical Report.
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