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Boundary-layer electron profiles for entry of a blunts slender body at high altitudeNew calculations of boundary-layer electron concentration profiles for entry of a blunt-nosed slender body into the earth's atmosphere are compared with previous calculations in which ambipolar diffusion was neglected. The old and new results agree in those flight regimes where ambipolar diffusion is unimportant, but large differences are noted in both peak electron concentration and profile shape at the higher altitudes, where diffusion effects are greatest. The new results are also compared with flight-measured profiles and with calculated profiles for a viscous-shock-layer theory which was recently reported in the literature. The boundary-layer results and the data agree in most respects. Differences which occur between predicted results and the data in the outer parts of the profile are discussed in terms of the effects of aerodynamic heating of the probes.
Document ID
19730018893
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Evans, J. S.
(NASA Langley Research Center Hampton, VA, United States)
Schexnayder, C. J., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Huber, P. W.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1973
Subject Category
Physics, Plasma
Report/Patent Number
NASA-TN-D-7332
Report Number: NASA-TN-D-7332
Accession Number
73N27620
Funding Number(s)
PROJECT: RTOP 501-04-03-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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