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

APA Citation

Dowell, E. H.., Air Force Flight Dynamics Laboratory (U.S.)., United States. Air Force. Systems Command. Aeronautical Systems Division., Boeing Company. (1965). Experimental and theoretical panel flutter studies in the mach number range of 1.0 to 5.0: supplement 1. Wright-Patterson Air Force Base, Ohio: Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force.

MLA Citation

Dowell, E. H., Air Force Flight Dynamics Laboratory (U.S.), United States. Air Force. Systems Command. Aeronautical Systems Division, and Boeing Company. Experimental And Theoretical Panel Flutter Studies In the Mach Number Range of 1.0 to 5.0: Supplement 1. Wright-Patterson Air Force Base, Ohio: Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965.

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