NASA technical notes. D-387. Effect of streamline contouring in wing-fuselage juncture in combination with supersonic area rule on sweptback-wing-fuselage configuration of high fineness ratio [with list of references]; by Charles D. Trescot, jr.
Publication Title:
Effect of streamline contouring in wing-fuselage juncture in combination with supersonic area rule on sweptback-wing-fuselage configuration of high fineness ratio [with list of references]; by Charles D. Trescot, jr.
Display Title:
NASA technical notes. D-387. Effect of streamline contouring in wing-fuselage juncture in combination with supersonic area rule on sweptback-wing-fuselage configuration of high fineness ratio [with list of references]; by Charles D. Trescot, jr.
Series Title:
NASA technical notes.
Corporate Agency Authors:
National Aeronautics and Space Administration
Sort Author:
National Aeronautics and Space Administration
Authors:
Trescot, Charles D. jr.
Date:
May 1960
Publish Date ISO Format:
1960-05-01T00:00:00Z
Publication Start:
19600501
Publication End:
19600531
Corporate/Agency Author:
National Aeronautics and Space Administration
Publication month:
8
Publication year:
1960
SuDoc number:
NAS 1.14:(nos.)
Description:
cover title, 19 p.+[2] leaves il. 4°
Notes:
[Processed.]
Notes:
[Processed.] Φ For Sale by OTS, Commerce Dept. Paper, 50c.