1. Experimental and theoretical panel flutter studies in the Mach number range 1·0 to 5·0;Dowell;ASD-TDR-63-449, USAF,1963
2. Experimental and theoretical panel flutter studies in the Mach number range 1·0 to 5·0;Dowell;A.I.A.A.J.,1965
3. Comparative experimental and theoretical studies of the flutter of flat panels in a low supersonic flow;Lock;AFOSR TN 670, Guggenheim Aero. Lab., Calif. Inst. Tech.,1961