Numerical simulation of the interaction of jet and freestream flows in engine exhaust systems
Author:
Affiliation:
1. Boeing Aerospace Co., Seattle, Wash.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1978-144
Reference34 articles.
1. 72-154, 1972.
2. The influence of the computational mesh on accuracy for initial value problems with discontinuous or nonunique solutions
3. Computation of Two-Dimensional, Viscous Nozzle Flow
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. Navier-Stokes and Experimental Modeling of Blunt-Base Rocket Nozzle Flow;Turbulent Shear-Layer/Shock-Wave Interactions;1986
2. Navier-Stokes Solutions for an Axisymmetric Nozzle;AIAA Journal;1982-09
3. Navier-Stokes solutions for an axisymmetric nozzle;17th Joint Propulsion Conference;1981-07-27
4. Numerical Simulation of Multistream Nozzle Flows;AIAA Journal;1980-09
5. Numerical simulation of multi-stream nozzle flows;12th Fluid and Plasma Dynamics Conference;1979-07-23
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