Some low-speed wind-tunnel experiments pertaining to the longitudinal stability characteristics of a 35° swept-wing model and an unswept-wing model /
by Byron M. Jaquet.

Description

Main Author

Jaquet, Byron M.

Related Names

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

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, 1953.

Subjects

Stability of airplanes, Longitudinal.
Airplanes > Airplanes / Wings, Swept-back.
Airplanes > Airplanes / Wings.
Airplanes > Airplanes / Wings.
Airplanes > Airplanes / Wings, Swept-back.
Stability of airplanes, Longitudinal.

Note

"October 20, 1953."

Physical Description

43 pages : illustrations ; 27 cm.

Locate a Print Version

Find in a library

Viewability