Wind-tunnel investigation at high subsonic speeds to determine the rolling derivatives of two wing-fuselage combinations having triangular winds, including a semiempirical method of estimating the rolling derivatives /
by James W. Wiggins.

Description

Main Author

Wiggins, James W.

Related Names

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

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, 1954.

Subjects

Airplanes > Airplanes / Wings, Triangular.
Rolling (Aerodynamics)

Note

On front cover: "February 81954."

Physical Description

32 pages : illustrations ; 27 cm.

Locate a Print Version

Find in a library

Viewability