A STUDY OF THE BENDING-TORSION AEROELASTIC MODES FOR AIRCRAFT WINGS

[1] BUROW H, 1948, FTS765RE US AIR FORC

[2] Carslaw H.S., 1941, OPERATIONAL METHODS

[3] GOLAND M, 1948, J APPLIED MECHANICS, V15

[4] JONES RT, 1938, NACA TN667

[5] MYKLESTAD N, 1944, VIBRATION ANAL

[6] SMILG B, 1942, 4798 US ARM AIR FORC

[7] THEODORSEN T, 1935, NACA TR496

[8] VON KARMAN T., 1938, J AERONAUTICAL SCI, V5

[9] WAGNER H, 1925, ZAMM, V5

[1] BUROW H, 1948, FTS765RE US AIR FORC

[2] Carslaw H.S., 1941, OPERATIONAL METHODS

[3] GOLAND M, 1948, J APPLIED MECHANICS, V15

[4] JONES RT, 1938, NACA TN667

[5] MYKLESTAD N, 1944, VIBRATION ANAL

[6] SMILG B, 1942, 4798 US ARM AIR FORC

[7] THEODORSEN T, 1935, NACA TR496

[8] VON KARMAN T., 1938, J AERONAUTICAL SCI, V5

[9] WAGNER H, 1925, ZAMM, V5