Technical notes. 3327. Approximate effect of leading-edge thickness, incidence angle, and inlet Mach number on inlet losses for high-solidity cascades of low cambered blades [with list of references]; by Linwood C. Wright.
Publication Title:
Approximate effect of leading-edge thickness, incidence angle, and inlet Mach number on inlet losses for high-solidity cascades of low cambered blades [with list of references]; by Linwood C. Wright.
Display Title:
Technical notes. 3327. Approximate effect of leading-edge thickness, incidence angle, and inlet Mach number on inlet losses for high-solidity cascades of low cambered blades [with list of references]; by Linwood C. Wright.
Series Title:
Technical notes.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Wright, Linwood C.
Date:
Dec. 1954
Publish Date ISO Format:
1954-12-01T00:00:00Z
Publication Start:
19541201
Publication End:
19541231
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
1
Publication year:
1954
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:6/(nos.)
Description:
cover title, 38+[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.