SUPERSONIC PANEL FLUTTER OF A CYLINDRICAL SHELL OF FINITE LENGTH

[1] ARNOLD RN, 1949, P ROYAL SOCIETY LO A, V197, P249

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

[3] DONNELL LH, 1933, NACA479 REP

[4] EISLEY JG, CALTECH AFOSR TN5523

[5] Flugge W., 1934, STATIK DYNAMIK SCHAL

[6] ON 2-DIMENSIONAL PANEL FLUTTER [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1958, 25 (03): : 145 - 160

[7] GOLDENVEIZER AL, 1953, TEORIIA UPRUGIKH TON

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

[9] FLUTTER OF RECTANGULAR SIMPLY SUPPORTED PANELS AT HIGH SUPERSONIC SPEEDS [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1957, 24 (08): : 563 - &

[10] HEDGEPETH JM, 1956, J AERONAUT SCI, V23, P609

[1] ARNOLD RN, 1949, P ROYAL SOCIETY LO A, V197, P249

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

[3] DONNELL LH, 1933, NACA479 REP

[4] EISLEY JG, CALTECH AFOSR TN5523

[5] Flugge W., 1934, STATIK DYNAMIK SCHAL

[6] ON 2-DIMENSIONAL PANEL FLUTTER [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1958, 25 (03): : 145 - 160

[7] GOLDENVEIZER AL, 1953, TEORIIA UPRUGIKH TON

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

[9] FLUTTER OF RECTANGULAR SIMPLY SUPPORTED PANELS AT HIGH SUPERSONIC SPEEDS [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1957, 24 (08): : 563 - &

[10] HEDGEPETH JM, 1956, J AERONAUT SCI, V23, P609