Effects of an inset tab on the hinge-moment and effectiveness characteristics of an unswept trailing-edge control on a 60° delta wing at Mach numbers from 0.75 to 1.96 /
by Lawrence D. Guy and Hoyt V. Brown.

Description

Main Author

Guy, Lawrence D. (Lawrence Duncan), 1921-

Related Names

Brown, Hoyt V.
United States. National Advisory Committee for Aeronautics.

Language(s)

English

Published

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

Subjects

Trailing edges (Aerodynamics)
Trailing edge flaps.
Hinge moments (Aerodynamics)
Airplanes > Airplanes / Wings, Triangular.
Airplanes > Airplanes / Control systems > Airplanes / Control systems / Testing.
Trailing edges (Aerodynamics)
Airplanes > Airplanes / Wings, Triangular.
Trailing edge flaps.
Hinge moments (Aerodynamics)
Airplanes > Airplanes / Control systems > Airplanes / Control systems / Testing.

Note

"Classification changed to unclassified, authority: NASA publication annoucement no. 3, effective date: December 3, 1958"--Stamped on cover.
"Confidential."
"February, 15, 1955."
Cover title.

Physical Description

35 pages : illustrations ; 27 cm.

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