Technical notes. 3944. Integral solution to flat-plate laminar boundary-layer flow existing inside and after expansion waves and after shock waves moving into quiescent fluid with particular application to complete shock-tube flow [with list of references]; by Robert L. Trimpi and Nathaniel B. Cohen.
Publication Title:
Integral solution to flat-plate laminar boundary-layer flow existing inside and after expansion waves and after shock waves moving into quiescent fluid with particular application to complete shock-tube flow [with list of references]; by Robert L. Trimpi and Nathaniel B. Cohen.
Display Title:
Technical notes. 3944. Integral solution to flat-plate laminar boundary-layer flow existing inside and after expansion waves and after shock waves moving into quiescent fluid with particular application to complete shock-tube flow [with list of references]; by Robert L. Trimpi and Nathaniel B. Cohen.
Series Title:
Technical notes.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Trimpi, Robert L. and Cohen, Nathaniel B.
Date:
June 1957
Publish Date ISO Format:
1957-06-01T00:00:00Z
Publication Start:
19570601
Publication End:
19570630
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
7
Publication year:
1957
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:6/(nos.)
Description:
cover title, ii+180+[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.