TABLES OF THE THEODORSEN CIRCULATION FUNCTION FOR GENERALIZED MOTION

[1] BIOT MA, 1942, 5 REP

[2] DIETZE F, 1943, ZWB FB1733

[3] THE QUASI-STEADY AIR FORCES FOR USE IN LOW-FREQUENCY STABILITY CALCULATIONS [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1950, 17 (10): : 601 - &

[4] A STUDY OF THE BENDING-TORSION AEROELASTIC MODES FOR AIRCRAFT WINGS [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1949, 16 (07): : 389 - 396

[5] JONES WP, 1945, R M2117

[6] KASSNER R, 1937, J ROYAL AERO SOC, V41

[7] LUKE YL, 1949, R111E108 MIDW RES I

[8] A NOTE ON A SOLUTION TO POSSIO INTEGRAL EQUATION FOR AN OSCILLATING AIRFOIL IN SUBSONIC FLOW [J]. QUARTERLY OF APPLIED MATHEMATICS, 1949, 7 (02) : 213 - 216

[9] RAUSCHER M, 1949, THEORETICAL EXPT MET, V6, P57

[10] REISSNER E, 1947, NACA TN1195

[1] BIOT MA, 1942, 5 REP

[2] DIETZE F, 1943, ZWB FB1733

[3] THE QUASI-STEADY AIR FORCES FOR USE IN LOW-FREQUENCY STABILITY CALCULATIONS [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1950, 17 (10): : 601 - &

[4] A STUDY OF THE BENDING-TORSION AEROELASTIC MODES FOR AIRCRAFT WINGS [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1949, 16 (07): : 389 - 396

[5] JONES WP, 1945, R M2117

[6] KASSNER R, 1937, J ROYAL AERO SOC, V41

[7] LUKE YL, 1949, R111E108 MIDW RES I

[8] A NOTE ON A SOLUTION TO POSSIO INTEGRAL EQUATION FOR AN OSCILLATING AIRFOIL IN SUBSONIC FLOW [J]. QUARTERLY OF APPLIED MATHEMATICS, 1949, 7 (02) : 213 - 216

[9] RAUSCHER M, 1949, THEORETICAL EXPT MET, V6, P57

[10] REISSNER E, 1947, NACA TN1195