Nonequilibrium blunt-body flow using the method of integral relations
Author:
Affiliation:
1. Massachusetts Institute of Technology, Cambridge, Mass
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.2493
Reference20 articles.
1. A CONTRIBUTION TO THE SOLUTION OF MIXED PROBLEMS OF TRANSONIC AERODYNAMICS
2. Belotserkovskii, O M"Flow past a circular cylinder with a detached shock wave/ Avco-RAD 9-TM59-66 (September 30,1959)
3. Non-equilibrium flow of an ideal dissociating gas
4. Ellington, D , "Approximate method for hypersonic nonequilibrium blunt body airflows,JAIAA J 1, 190 (1963)
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1. On stagnation-point conditions in non-equilibrium inviscid blunt-body flows;Journal of Fluid Mechanics;1970-08-17
2. Symmetrical, equilibrium flow past a blunt body at superorbital re-entry speeds.;AIAA Journal;1967-04
3. Use of the method of integral relations for the determination of theconvective heat flux to a reentry body.;AIAA Journal;1966-05
4. A theoretical study of non-equilibrium blunt-body flows;Journal of Fluid Mechanics;1966-01
5. Characteristic calculation of flowfields with chemical reactions.;AIAA Journal;1966-01
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