Improved method for solving the viscous shock layer equations
Author:
Affiliation:
1. Texas A&M University, College Station, Texas 77843
2. University of Cincinnati, Cincinnati, Ohio 45221
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.11135
Reference21 articles.
1. Second-order boundary-layer effects in hypersonic flow past axisymmetric blunt bodies
2. Hypersonic Merged Stagnation Shock Layers Part I: Adiabatic Wall Case
Cited by 2 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. A new method for solution of viscous shock-layer equations;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2009-12-17
2. The comparative analysis of approximate numerical solutions of the Navier-Stokes equations;14th Applied Aerodynamics Conference;1996-06-17
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