FLUTTER OF RECTANGULAR SIMPLY SUPPORTED PANELS AT HIGH SUPERSONIC SPEEDS

[1] PISTON THEORY - A NEW AERODYNAMIC TOOL FOR THE AEROELASTICIAN [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1956, 23 (12): : 1109 - 1118

[2] Bisplinghoff R. L., 1956, VIBRATIONS THERMALLY

[3] EISLEY JG, 1955, GALCIT OSRTN55236 RE

[4] EISLEY JG, 1956, GALCIT OSRTN56296 RE

[5] EVVARD JC, 1950, NACA REPORT, V951

[6] THE STATIC STABILITY OF A 2-DIMENSIONAL CURVED PANEL IN A SUPERSONIC FLOW, WITH AN APPLICATION TO PANEL FLUTTER [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1954, 21 (08): : 556 - 565

[7] FUNG YC, 1955, GALCIT OSRTN55237 RE

[8] AN EXACT SOLUTION FOR 2-DIMENSIONAL LINEAR PANEL FLUTTER AT SUPERSONIC SPEEDS [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1954, 21 (04): : 275 - 276

[9] GOLAND M, 1954, J AERONAUTICAL SCI, V21, P276

[10] HAYES WD, 1950, AL1029 N AM AV REP

[1] PISTON THEORY - A NEW AERODYNAMIC TOOL FOR THE AEROELASTICIAN [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1956, 23 (12): : 1109 - 1118

[2] Bisplinghoff R. L., 1956, VIBRATIONS THERMALLY

[3] EISLEY JG, 1955, GALCIT OSRTN55236 RE

[4] EISLEY JG, 1956, GALCIT OSRTN56296 RE

[5] EVVARD JC, 1950, NACA REPORT, V951

[6] THE STATIC STABILITY OF A 2-DIMENSIONAL CURVED PANEL IN A SUPERSONIC FLOW, WITH AN APPLICATION TO PANEL FLUTTER [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1954, 21 (08): : 556 - 565

[7] FUNG YC, 1955, GALCIT OSRTN55237 RE

[8] AN EXACT SOLUTION FOR 2-DIMENSIONAL LINEAR PANEL FLUTTER AT SUPERSONIC SPEEDS [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1954, 21 (04): : 275 - 276

[9] GOLAND M, 1954, J AERONAUTICAL SCI, V21, P276

[10] HAYES WD, 1950, AL1029 N AM AV REP