Experimental and theoretical panel flutter studies in the mach number range of 1.0 to 5.0 :
supplement 1 /
E. H. Dowell.

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Main Author: Dowell, E. H.
Related Names: Air Force Flight Dynamics Laboratory (U.S.)
United States. Air Force.
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, 1965.
Subjects: Vibration > Vibration / Testing.
Mach number.
Flutter (Aerodynamics)
Note: "Project No. 1370, Task No. 137003."
"August 1965."
Physical Description: v, 16 pages : illustrations ; 28 cm.
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