Jet effects on longitudinal trim of an airplane configuration measured at Mach numbers between 1.2 and 1.8 /
by Robert F. Peck.

Description

Main Author

Peck, Robert F.

Related Names

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

Language(s)

English

Published

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

Subjects

Stability of airplanes, Longitudinal.

Note

On front cover: "Classification Changed to Unclassified, Authority: NACA Research Abstract No. 121. Effective Date; October 17, 1957 WHL."
On front cover: "January 18, 1955."

Physical Description

17 pages : illustrations ; 27 cm.

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