Symmetrical, equilibrium flow past a blunt body at superorbital re-entry speeds.
Author:
Affiliation:
1. Philco Corporation, Newport Beach, Calif.
2. University of California at Berkeley, Berkeley, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.4037
Reference37 articles.
1. A THEORY OF ASYMMETRIC HYPERSONIC BLUNT-BODY FLOWS
2. Blunt-Nose Inviscid Airflows With Coupled Nonequilibrium Processes
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. Chapter 4 Applications to Fluid Mechanics;The Method of Weighted Residuals and Variational Principles - With Application in Fluid Mechanics, Heat and Mass Transfer;1972
2. PREDICTION OF THERMAL FLUXES TO VERY BLUNT PLANETARY ENTRY VEHICLES BY THE INTEGRAL METHOD;Proceedings of the XXth International Astronautical Congress;1972
3. Approximate method for considering real gas effects in hypersonic flow about segmental bodies;Fluid Dynamics;1972
4. RADIATING FLOWS DURING ENTRY INTO PLANETARY ATMOSPHERES;Propulsion Re-Entry Physics;1970
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