NACA research memorandum RM (series). L57I10. Aerodynamic characteristics at Mach number of 4.06 of typical supersonic airplane model using body and vertical-tail wedges to improve directional stability [with list of references]; by Hubert W. Dunning.
Publication Title:
Aerodynamic characteristics at Mach number of 4.06 of typical supersonic airplane model using body and vertical-tail wedges to improve directional stability [with list of references]; by Hubert W. Dunning.
Display Title:
NACA research memorandum RM (series). L57I10. Aerodynamic characteristics at Mach number of 4.06 of typical supersonic airplane model using body and vertical-tail wedges to improve directional stability [with list of references]; by Hubert W. Dunning.
Series Title:
NACA research memorandum RM (series).
Corporate Agency Authors:
National Aeronautics and Space Administration
Sort Author:
National Aeronautics and Space Administration
Authors:
Dunning, Hubert W.
Date:
Dec. 3, 1957
Publish Date ISO Format:
1957-12-03T00:00:00Z
Publication Start:
19571203
Publication End:
19571203
Corporate/Agency Author:
National Aeronautics and Space Administration
Publication month:
1
Publication year:
1957
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:15/(letter-nos.)
Description:
cover title, 38 p. + [2] leaves, il. 4°
Notes:
[Classification changed Feb. 8, 1960.] and (National Advisory committee for Aeronautics.) [Processed. No longer confidential.]
Notes:
(National Advisory committee for Aeronautics.) [Processed. No longer confidential.] † Distribution Made by Issuing Office.