Technical notes. 2986. Effect of blade-thickness taper on axial-velocity distribution at leading edge of entrance rotor-blade row with axial inlet, and influence of this distribution on alinement of rotor blade for zero angle of attack [with list of references]; by John D. Stanitz.
Publication Title:
Effect of blade-thickness taper on axial-velocity distribution at leading edge of entrance rotor-blade row with axial inlet, and influence of this distribution on alinement of rotor blade for zero angle of attack [with list of references]; by John D. Stanitz.
Display Title:
Technical notes. 2986. Effect of blade-thickness taper on axial-velocity distribution at leading edge of entrance rotor-blade row with axial inlet, and influence of this distribution on alinement of rotor blade for zero angle of attack [with list of references]; by John D. Stanitz.
Series Title:
Technical notes.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Stanitz, John D.
Date:
Aug. 1953
Publish Date ISO Format:
1953-08-01T00:00:00Z
Publication Start:
19530801
Publication End:
19530831
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
5
Publication year:
1953
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:6/(nos.)
Description:
cover title, 33+[4] p. il. 4°
Notes:
[The 4 pages in the collation consist of detachable catalog entries on heavy paper designed to be used in a card catalog.] and [Processed.]
Notes:
[Processed.] † Distribution Made by Issuing Office.