NASA memorandum. 5-26-59L. Modified matrix method for calculating steady-state span loading on flexible wings in subsonic flight [with list of references]; by Patrick A. Gainer and William S. Aiken, jr.
Publication Title:
Modified matrix method for calculating steady-state span loading on flexible wings in subsonic flight [with list of references]; by Patrick A. Gainer and William S. Aiken, jr.
Display Title:
NASA memorandum. 5-26-59L. Modified matrix method for calculating steady-state span loading on flexible wings in subsonic flight [with list of references]; by Patrick A. Gainer and William S. Aiken, jr.
Series Title:
NASA memorandum.
Corporate Agency Authors:
National Aeronautics and Space Administration
Sort Author:
National Aeronautics and Space Administration
Authors:
Gainer, Patrick A. and Aiken, William S. jr.
Date:
June 1959
Publish Date ISO Format:
1959-06-01T00:00:00Z
Publication Start:
19590601
Publication End:
19590630
Corporate/Agency Author:
National Aeronautics and Space Administration
Publication month:
7
Publication year:
1959
Publication place:
Washington
SuDoc number:
NAS 1.10:(nos.)
Description:
cover title, 62 p.+[2] leaves, 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.