NASA technical report R (series). 163. Hypersonic shock-heated flow parameters for velocities to 46,000 feet per second and altitudes to 323,000 feet [with list of references]; by Paul W. Huber.

Publication Title:
Hypersonic shock-heated flow parameters for velocities to 46,000 feet per second and altitudes to 323,000 feet [with list of references]; by Paul W. Huber.
Display Title:
NASA technical report R (series). 163. Hypersonic shock-heated flow parameters for velocities to 46,000 feet per second and altitudes to 323,000 feet [with list of references]; by Paul W. Huber.
Series Title:
NASA technical report R (series).
Corporate Agency Authors:
National Aeronautics and Space Administration
Sort Author:
National Aeronautics and Space Administration
Authors:
Huber, Paul W.
Date:
Dec. 1963 [published 1964]
Publish Date ISO Format:
1964-01-01T00:00:00Z
Publication Start:
19640101
Publication End:
19641231
Corporate/Agency Author:
National Aeronautics and Space Administration
Publication month:
13
Publication year:
1964
SuDoc number:
NAS 1.12:(nos.)
Description:
cover title, [1]+74+[1] p. il. 4°
Notes:
Φ For Sale by OTS, Commerce Dept. Paper, $2.00.
Availability:
Φ For Sale by OTS, Commerce Dept. Paper, $2.00.
Monthly Catalog date:
August 1964
Monthly Catalog issue number:
835
Monthly Catalog page number:
1
Monthly Catalog issue date:
1964-08-01T00:00:00Z
Monthly Catalog entry number:
14900
Record start page number:
76

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