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

APA Citation

Dowell, E. H.., Voss, H. M.., Air Force Flight Dynamics Laboratory (U.S.)., Boeing Company. (1963). Experimental and theoretical panel flutter studies in the mach number range of 1.0 to 5.0. 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., H. M. Voss, Air Force Flight Dynamics Laboratory (U.S.), and Boeing Company. Experimental And Theoretical Panel Flutter Studies In the Mach Number Range of 1.0 to 5.0. Wright-Patterson Air Force Base, Ohio: Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1963.