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Pressures, forces, moments and shock shapes for a geometrically matched sphere-cone and hyperboloid at Mach 20.3 in heliumAn investigation was conducted to compare measured and predicted pressure distributions, forces and moments, and shock shapes on a geometrically matched sphere-cone and hyperboloid. A hyperboloid with a nose radius of 0.5276 in. and an asymptotic angle of 39.9871 deg was matched to a sphere-cone with a nose radius of 0.750 in. and a cone half-angle of 45 deg. Experimental results in helium at a free-stream Mach number of 20.3 and a free-stream unit Reynolds number of 6.83 x 10 to the 6th power per foot were combined with predicted results from a theoretical method to compare the two shapes. Comparisons of experimental results showed small differences in the two shapes, but the prediction method provided better results for the hyperboloid than for the sphere-cone.
Document ID
19830008404
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Calloway, R. L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1983
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
L-15499
NASA-TP-2100
NAS 1.60:2100
Report Number: L-15499
Report Number: NASA-TP-2100
Report Number: NAS 1.60:2100
Accession Number
83N16675
Funding Number(s)
PROJECT: RTOP 506-51-13-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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