SOME RESULTS OF SWEPTBACK WING STRUCTURAL STUDIES

[1] BISPLINGHOFF RL, 1949, INVESTIGATION DEFORM

[2] GOODMAN S, 1950, ROOT STRESS DISTRIBU

[3] HELDENFELS RR, 1950, NACA TN2232

[4] KUHN P, 1942, NACA L352 WART REP

[5] KUHN P, 1947, NACA TN1361

[6] COMPUTATION OF INFLUENCE COEFFICIENTS FOR AIRCRAFT STRUCTURES WITH DISCONTINUITIES AND SWEEPBACK [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1947, 14 (10): : 547 - 560

[7] THOMPSON JJ, 1949, ACA43 COMM AUSTR AER

[8] WITTRICK WH, 1948, ACA39 COMM AUSTR AER

[9] ZENDER G, 1950, NACA TN2054

[10] ZENDER G, 1948, NACA TN1525

[1] BISPLINGHOFF RL, 1949, INVESTIGATION DEFORM

[2] GOODMAN S, 1950, ROOT STRESS DISTRIBU

[3] HELDENFELS RR, 1950, NACA TN2232

[4] KUHN P, 1942, NACA L352 WART REP

[5] KUHN P, 1947, NACA TN1361

[6] COMPUTATION OF INFLUENCE COEFFICIENTS FOR AIRCRAFT STRUCTURES WITH DISCONTINUITIES AND SWEEPBACK [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1947, 14 (10): : 547 - 560

[7] THOMPSON JJ, 1949, ACA43 COMM AUSTR AER

[8] WITTRICK WH, 1948, ACA39 COMM AUSTR AER

[9] ZENDER G, 1950, NACA TN2054

[10] ZENDER G, 1948, NACA TN1525