Technical notes. 2729. Analysis of supersonic flow in region of leading edge of curved airfoils, including charts for determining surface-pressure gradient and shock-wave curvature [with list of references]; by Samuel Kraus.
Publication Title:
Analysis of supersonic flow in region of leading edge of curved airfoils, including charts for determining surface-pressure gradient and shock-wave curvature [with list of references]; by Samuel Kraus.
Display Title:
Technical notes. 2729. Analysis of supersonic flow in region of leading edge of curved airfoils, including charts for determining surface-pressure gradient and shock-wave curvature [with list of references]; by Samuel Kraus.
Series Title:
Technical notes.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Kraus, Samuel
Date:
June 1952
Publish Date ISO Format:
1952-06-01T00:00:00Z
Publication Start:
19520601
Publication End:
19520630
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
7
Publication year:
1952
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:6/(nos.)
Description:
cover title, 45+[4] p. il. 4°
Notes:
[Processed.]
Notes:
[Processed.] † Distribution Made by Issuing Office.