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Hypersonic rarefied flow over sharp slender conesDrag, heat transfer, and number flux were measured on sharp cones in the near free, molecule flow regime, and the results were compared with available Monte Carlo calculations. In general, the calculations predicted the magnitude of the data; however, the heat transfer and drag increased with increasing Knudsen number at a faster rate than predicted. Also the drag coefficients measured for the slender cones at high Knudsen number were higher than predicted for free molecule flow. These disagreements between theory and experiment could possibly be attributed to the simplicity of the surface interaction laws assumed in the theory. Reynolds analogy factors obtained from the experimental measurements agreed with free-molecule values and also with that obtained by the Monte Carlo technique.
Document ID
19720010639
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Kussoy, M. I.
(NASA Ames Research Center Moffett Field, CA, United States)
Stewart, D. A.
(NASA Ames Research Center Moffett Field, CA, United States)
Hortsman, C. C.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1972
Subject Category
Fluid Mechanics
Report/Patent Number
A-4133
NASA-TN-D-6689
Report Number: A-4133
Report Number: NASA-TN-D-6689
Accession Number
72N18289
Funding Number(s)
PROJECT: RTOP 129-01-20-01-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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