Technical report R (series), 1961. 85. 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 report R (series), 1961. 85. 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 report R (series), 1961.
Corporate Agency Authors:
National Aeronautics and Space Administration
Sort Author:
National Aeronautics and Space Administration
Authors:
Trimpi, Robert L. and Cohen, Nathaniel B.
Date:
[1961.]
Publish Date ISO Format:
1961-01-01T00:00:00Z
Publication Start:
19610101
Publication End:
19611231
Corporate/Agency Author:
National Aeronautics and Space Administration
Publication month:
13
Publication year:
1961
SuDoc number:
NAS 1.12:(nos.)
Description:
cover title, i+56 p.+[2] leaves, il. 4°
Notes:
[Supersedes NACA technical note 4347, 1958.]
Notes:
[Supersedes NACA technical note 4347, 1958.] * For Sale by Superintendent of Documents. Paper, $15.00 a yr., $4.00 additional for foreign mailing; single copies vary in price. • Sent to Depository Libraries. Item 830-D
Availability:
* For Sale by Superintendent of Documents. Paper, 50c. and * For Sale by Superintendent of Documents. Paper, $15.00 a yr., $4.00 additional for foreign mailing; single copies vary in price. • Sent to Depository Libraries. Item 830-D