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The effects of shock wave precursors ahead of hypersonic entry vehiclesA model has been developed to predict the magnitude and characteristics of the shock wave precursor ahead of a hypervelocity vehicle. This model includes both chemical and thermal nonequilibrium, utilizes detailed mass production rates for the photodissociation and photoionization reactions, and accounts for the effects of radiative absorption and emission on the individual internal energy modes of both atomic and diatomic species. Comparison of the present results with shock tube data indicates that the model is reasonably accurate. A series of test cases representing earth aerocapture return from Mars indicate that there is significant production of atoms, ions and electrons ahead of the shock front due to radiative absorption and that the precursor is characterized by an enhanced electron/electronic temperature and molecular ionization. However, the precursor has a negligible effect on the shock layer flow field.
Document ID
19910057896
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stanley, Scott A.
(Texas A&M Univ. College Station, TX, United States)
Carlson, Leland A.
(Texas A & M University College Station, United States)
Date Acquired
August 15, 2013
Publication Date
June 1, 1991
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 91-1465
Accession Number
91A42519
Funding Number(s)
CONTRACT_GRANT: NAG1-1003
Distribution Limits
Public
Copyright
Other

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