Technical notes. 4347. Nonlinear theory for predicting effects of unsteady laminar, turbulent, or transitional boundary layers on attenuation of shock waves in shock tube with experimental comparison [with list of references]; by Robert L. Trimpi and Nathaniel B. Cohen.
Publication Title:
Nonlinear theory for predicting effects of unsteady laminar, turbulent, or transitional boundary layers on attenuation of shock waves in shock tube with experimental comparison [with list of references]; by Robert L. Trimpi and Nathaniel B. Cohen.
Display Title:
Technical notes. 4347. Nonlinear theory for predicting effects of unsteady laminar, turbulent, or transitional boundary layers on attenuation of shock waves in shock tube with experimental comparison [with list of references]; by Robert L. Trimpi and Nathaniel B. Cohen.
Series Title:
Technical notes.
Corporate Agency Authors:
National Aeronautics and Space Administration
Sort Author:
National Aeronautics and Space Administration
Authors:
Trimpi, Robert L. and Cohen, Nathaniel B.
Date:
Sept. 1958
Publish Date ISO Format:
1958-09-01T00:00:00Z
Publication Start:
19580901
Publication End:
19580930
Corporate/Agency Author:
National Aeronautics and Space Administration
Publication month:
4
Publication year:
1958
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:6/(nos.)
Description:
cover title, 105+[6] p. il. 4°
Notes:
[Processed. The pages or leaves in brackets in each collation consist of detachable card catalog entries.]
Notes:
[Processed. The pages or leaves in brackets in each collation consist of detachable card catalog entries.] † Distribution Made by Issuing Office.