STRUCTURAL ANALYSIS AND INFLUENCE COEFFICIENTS FOR DELTA-WINGS

[1] BISCH PE, 1948, NA48310 N AM AV REP

[2] BISPLINGHOFF RL, 1949, INVESTIGATION DEFORM

[3] HOUBOLT JC, 1950, NACA TN2060

[4] LEVY S, 1953, J APPL MECH-T ASME, V20, P131

[5] A SIMPLE TABULAR METHOD OF CALCULATING DEFLECTIONS AND INFLUENCE COEFFICIENTS OF BEAMS [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1946, 13 (01): : 23 - 28

[6] REISSNER E, 1951, NACA TN2369

[7] SCHUERCH H, 1952, AERONAUTICAL ENG REV, V11, P34

[8] SCHUERCH HU, 1950, 2 I FLUGZ FLUGZ ETH

[9] STEIN M, 1952, NACA TN2621

[10] Timoshenko SP, 1934, THEORY ELASTICITY

[1] BISCH PE, 1948, NA48310 N AM AV REP

[2] BISPLINGHOFF RL, 1949, INVESTIGATION DEFORM

[3] HOUBOLT JC, 1950, NACA TN2060

[4] LEVY S, 1953, J APPL MECH-T ASME, V20, P131

[5] A SIMPLE TABULAR METHOD OF CALCULATING DEFLECTIONS AND INFLUENCE COEFFICIENTS OF BEAMS [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1946, 13 (01): : 23 - 28

[6] REISSNER E, 1951, NACA TN2369

[7] SCHUERCH H, 1952, AERONAUTICAL ENG REV, V11, P34

[8] SCHUERCH HU, 1950, 2 I FLUGZ FLUGZ ETH

[9] STEIN M, 1952, NACA TN2621

[10] Timoshenko SP, 1934, THEORY ELASTICITY