An engineering model for reentry vehicle turbulent wakes - Applications to electron density prediction and decelerator performance
Author:
Affiliation:
1. Aerospace Corp., El Segundo, Calif.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1979-153
Reference21 articles.
1. Atkinson, C.A. and W.W. Haigh, "Decelerator Performance Study-Final Report, 'I SAMSO-TR-70-48, Mar. 1970.
2. English, E. A."Nosetip Recovery Vehicle Postflight Development Report, I' SAND 75-8059, Jan. 1976 (unlimited releasc).
3. The application of finite difference methods to the supersonic near wake
4. Ohrenberger, J.T. and E. Baum, "A Theoretical Model of the Near Wake of a Slender Body in Supersonic Flow, I' AIAA Journal, in(9), sept. 1972, pp.1165.11.
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