OPTIMIZATION OF COMPLEX STRUCTURES TO SATISFY FLUTTER REQUIREMENTS

[1] BEVERIDGE GS, 1970, OPTIMIZATION THEORY, P435

[2] STRUCTURAL OPTIMIZATION IN DYNAMICS RESPONSE REGIME - A COMPUTATIONAL APPROACH [J]. AIAA JOURNAL, 1970, 8 (10) : 1798 - &

[3] MCCART BR, 1969, AIAA STRUCTURAL DYNA, P23

[4] RUBIN CP, 1969, AIAA STRUCTURAL DYNA, P9

[5] SCANLAN RH, 1968, INTRO STUDY AIRCRAFT, P398

[6] SMILG B, 1942, TR4798 USAAF

[7] OPTIMIZATION OF STRUCTURES TO SATISFY FLUTTER REQUIREMENTS [J]. AIAA JOURNAL, 1969, 7 (05) : 945 - &

[1] BEVERIDGE GS, 1970, OPTIMIZATION THEORY, P435

[2] STRUCTURAL OPTIMIZATION IN DYNAMICS RESPONSE REGIME - A COMPUTATIONAL APPROACH [J]. AIAA JOURNAL, 1970, 8 (10) : 1798 - &

[3] MCCART BR, 1969, AIAA STRUCTURAL DYNA, P23

[4] RUBIN CP, 1969, AIAA STRUCTURAL DYNA, P9

[5] SCANLAN RH, 1968, INTRO STUDY AIRCRAFT, P398

[6] SMILG B, 1942, TR4798 USAAF

[7] OPTIMIZATION OF STRUCTURES TO SATISFY FLUTTER REQUIREMENTS [J]. AIAA JOURNAL, 1969, 7 (05) : 945 - &