A low-speed investigation of a thin 60° delta wing equipped with a double slotted flap to determine the chordwise pressure distribution and the effect of vane size /
by Delwin R. Croom.

Description

Main Author

Croom, Delwin R.

Related Names

United States. National Adviosry Committee for Aeronautics.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, 1955.

Subjects

Delta wing airplanes > Delta wing airplanes / Aerodynamics > Delta wing airplanes / Aerodynamics / Testing.

Note

"March 8, 1955."
Cover title.

Physical Description

42 pages : illustrations ; 27 cm.

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