Technical notes. 3503. Reduction of profile drag at supersonic velocities by use of airfoil sections having blunt trailing edge [With list of references]; by Dean R. Chapman.
Publication Title:
Reduction of profile drag at supersonic velocities by use of airfoil sections having blunt trailing edge [With list of references]; by Dean R. Chapman.
Display Title:
Technical notes. 3503. Reduction of profile drag at supersonic velocities by use of airfoil sections having blunt trailing edge [With list of references]; by Dean R. Chapman.
Series Title:
Technical notes.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Chapman, Dean R.
Date:
Sept. 1955
Publish Date ISO Format:
1955-09-01T00:00:00Z
Publication Start:
19550901
Publication End:
19550930
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
4
Publication year:
1955
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:6/(nos.)
Description:
cover title, 29+[2] leaves, il. 4°
Notes:
[Supersedes declassified NACA RM A9H11, 1949.] and [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.