NASA technical note TN (series). D-5338. Dynamic response of Mach 2.5 axisymmetric inlet with engine or cold pipe and utilizing 60 percent supersonic internal area contraction [with list of referencesl; by Joseph F. Wasserbauer.

Publication Title:
Dynamic response of Mach 2.5 axisymmetric inlet with engine or cold pipe and utilizing 60 percent supersonic internal area contraction [with list of referencesl; by Joseph F. Wasserbauer.
Display Title:
NASA technical note TN (series). D-5338. Dynamic response of Mach 2.5 axisymmetric inlet with engine or cold pipe and utilizing 60 percent supersonic internal area contraction [with list of referencesl; by Joseph F. Wasserbauer.
Series Title:
NASA technical note TN (series).
Corporate Agency Authors:
National Aeronautics and Space Administration
Sort Author:
National Aeronautics and Space Administration
Authors:
Wasserbauer, Joseph F.
Author place:
Washington, DC
Author zip:
20546
Date:
July 1969
Publish Date ISO Format:
1969-07-01T00:00:00Z
Publication Start:
19690701
Publication End:
19690731
Corporate/Agency Author:
National Aeronautics and Space Administration
Publication month:
6
Publication year:
1969
SuDoc number:
NAS 1.14:D-(nos.)
Description:
cover title, ii+58 p. il. 4°
Notes:
Φ For Sale by OTS, Commerce Dept. Paper, $3.00.
Availability:
Φ For Sale by OTS, Commerce Dept. Paper, $3.00.
Monthly Catalog date:
September 1969
Monthly Catalog issue number:
896
Monthly Catalog page number:
1
Monthly Catalog issue date:
1969-09-01T00:00:00Z
Monthly Catalog entry number:
13116
Record start page number:
86

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