Calculation of axisymmetric inlet flowfield using the Euler equations
Author:
Affiliation:
1. McDonnell Douglas Research Laboratories, St. Louis, MO
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1983-1853
Reference14 articles.
1. Cartesian Mesh Solution for Axisymmetric Transonic Potential Flow Around Inlets
2. Reyhner, T. A, "Transonic Polentiol Flow Around Axisymmelric Inlels and Bodies 01 Angle-of-Arlack. I` AIAA Journal, Vol.15, Sepr. 1977,pp.1299-1306.
3. Reyhner, T. A, "Transonic Polenrial Flow Compulation Ahour Three-Dimensional Inlels, Ductr, and Bodies,`I AlAA Paper No. 80-1364, 1980.
4. Calculation of Transonic Flow around Axisymmetric Inlets
5. Accelerated Iterative Calculation of Transonic Nacelle Flowfields
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. Accurate solutions for transonic viscous flow over finite wings;4th Joint Fluid Mechanics, Plasma Dynamics and Lasers Conference;1986-05-12
2. Simulation of transonic three-dimensional nacelle/inlet flowfields using an Euler/Navier-Stokes algorithm;23rd Aerospace Sciences Meeting;1985-01-14
3. Grid generation techniques in computational fluid dynamics;AIAA Journal;1984-11
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