ON 2-DIMENSIONAL PANEL FLUTTER

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

[2] BROOKS JA, 1957, JAN P JOINT NYU IBM

[3] Courant R., 1943, B AM MATH SOC, V49, P1, DOI [DOI 10.1090/S0002-9904-1943-07818-4, 10.1090/S0002-9904-1943-07818-4]

[4] EISLEY JG, 1956, AF OSR TN56296

[5] EISLEY JG, 1955, AF OSR TN55236

[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, 1957, APR P MIDW C FLUID S

[8] FUNG YC, 1955, CALTECH ORS TN55237

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

[10] GOLAND M, 1955, J AERONAUTICAL SCI, V22, P656

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

[2] BROOKS JA, 1957, JAN P JOINT NYU IBM

[3] Courant R., 1943, B AM MATH SOC, V49, P1, DOI [DOI 10.1090/S0002-9904-1943-07818-4, 10.1090/S0002-9904-1943-07818-4]

[4] EISLEY JG, 1956, AF OSR TN56296

[5] EISLEY JG, 1955, AF OSR TN55236

[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, 1957, APR P MIDW C FLUID S

[8] FUNG YC, 1955, CALTECH ORS TN55237

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

[10] GOLAND M, 1955, J AERONAUTICAL SCI, V22, P656