Theoretical and experimental panel flutter studies in the Mach number range 1.0 to 5.0.
DOWELL, E. H., VOSS, H. M. /BOEING CO., AERO-SPACE DIV., SEATTLE, WASH./.
AIAA Journal ; 3 , 12 ; 2292-2304
1965-01-01
13 pages
Article (Journal)
Electronic Resource
English