Numerical stability of boundary layers with massive blowing.
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.6895
Reference9 articles.
1. The Homogeneous Boundary Layer at an Axisymmetric Stagnation Point With Large Rates of Injection
2. Boundary-layer flows with large injection and heat transfer.
3. Numerical analysis of stagnation point flows with massive blowing
4. Grenzen der Grenzschichtbeeinflussung
Cited by 9 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. Unsteady Compressible Three-Dimensional Stagnation Point Boundary Layers with Large Injection Rates;ZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik;1985
2. Compressible second-order boundary layers for three-dimensional stagnation point flows with mass transfer;International Journal of Engineering Science;1982-01
3. Hypersonic stagnation-point boundary layers with massive blowing in the presence of a magnetic field;Physics of Fluids;1979
4. Methods for Predicting Radiation-Coupled Flowfields about Planetary Entry Probes;Aerodynamic Heating and Thermal Protection Systems;1978-01-01
5. Fast and stable numerical method for boundary-layer flow with massive blowing;AIAA Journal;1976-01
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