Experimental and theoretical panel flutter studies in the mach number range of 1.0 to 5.0 /
E. H. Dowell and H. M. Voss.

Description

Main Author

Dowell, E. H.

Related Names

Voss, H. M., author.
Air Force Flight Dynamics Laboratory (U.S.)
Boeing Company

Language(s)

English

Published

Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1963.

Subjects

Vibration > Vibration / Testing.
Mach number.
Flutter (Aerodynamics)

Note

"Stamped: AD346621 (from http://www.dtic.mil)."
"(Prepared under Contract No. AF 33(616)-8081 by The Boeing Company, Seatlle 24, Washington)."
"Project No. 1370, Task No. 137002."
"December 1963."

Physical Description

xvi, 177 pages : illustrations, figures, tables ; 28 cm.

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