NASA technical memorandums. X-92. Effects of wing-crank, leading-edge chord extensions and horizontal-tall height on longitudinal stability of swept-wing models at Mach numbers from 0.6 to 1.4 [with list of references]; by Roy M. Wakefield.
Publication Title:
Effects of wing-crank, leading-edge chord extensions and horizontal-tall height on longitudinal stability of swept-wing models at Mach numbers from 0.6 to 1.4 [with list of references]; by Roy M. Wakefield.
Display Title:
NASA technical memorandums. X-92. Effects of wing-crank, leading-edge chord extensions and horizontal-tall height on longitudinal stability of swept-wing models at Mach numbers from 0.6 to 1.4 [with list of references]; by Roy M. Wakefield.
Series Title:
NASA technical memorandums.
Corporate Agency Authors:
National Aeronautics and Space Administration
Sort Author:
National Aeronautics and Space Administration
Authors:
Wakefield, Roy M.
Date:
Oct. 1959
Publish Date ISO Format:
1959-10-01T00:00:00Z
Publication Start:
19591001
Publication End:
19591031
Corporate/Agency Author:
National Aeronautics and Space Administration
Publication month:
3
Publication year:
1959
SuDoc number:
NAS 1.15:(letters-nos.)
Description:
cover title, 116 p. + [2] leaves, il. 4°
Notes:
[Processed. No longer confidential. Classification changed Sept. 1, 1961.]
Notes:
[Processed. No longer confidential. Classification changed Sept. 1, 1961.] † Distribution Made by Issuing Office.