Boundary layer flows on transonic projectiles
Author:
Affiliation:
1. U.S. Army, Ballistics Research Laboratory, Aberdeen Proving Ground, Md.
2. Delaware, University, Newark, Del.
3. Virginia Polytechnic Institute and State University, Blacksburg, Va.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1979-1551
Reference13 articles.
1. Pulliam, Thomas H. and Steger, Joseph L. "On Implicite Finite Difference Simulation of Three-Dimensional Flow," AIAA Paper 78-10.
2. Calculation of Transonic Flow over Supercritical Airfoil Sections
Cited by 4 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. Experimental study of supersonic turbulent flow on a blunted axisymmetric body;AIAA Journal;1986-05
2. Measurements on a projectile with an asymmetric afterbody at transonic speeds;21st Aerospace Sciences Meeting;1983-01-10
3. Transonic Flow Past Axisymmetric and Nonaxisymmetric Boatt ail Projectiles;AIAA Journal;1982-10
4. A theoretical and experimental investigation of a transonic projectile flow field;20th Aerospace Sciences Meeting;1982-01-11
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