Application of a supersonic Euler method to Pegasus aerodynamics
Author:
Affiliation:
1. Nielsen Engineering and Research, Inc., Mountain View, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1993-764
Reference5 articles.
1. Wardlaw, A.B.,Jr.,Baltakis,F.P., Martin, F. M., Priolo, F. J., and Jettmar, R. U. "Godunov's Method for SupersonicTactical Missiles,"AIAA85-1812, August 1985.
2. An integral boundary layer procedure for tactical missiles
3. Kuhn, G. D. "Postflight Aerothermodynamic Analysis of Pegasus Using ComputationalFluid DynamicsTechniques," NASA CR-186017,March,1992.
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. Recent Applications of Space-Marching Euler Solver NEARZEUSIN/ZEUSBL to Conventional and Airbreathing Missile Configurations;20th AIAA Applied Aerodynamics Conference;2002-06-24
2. Computational aerodynamic design and analysis of launch vehicles;38th Aerospace Sciences Meeting and Exhibit;2000-01-10
3. Aerodynamic analysis of Pegasus - Computations vs reality;31st Aerospace Sciences Meeting;1993-01-11
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