Optimal weight of cracked composite panels by an equivalent strain constraint
19th AIAA Applied Aerodynamics Conference ; 2001 ; Anaheim , CA , U.S.A.
2001-01-01
Conference paper
Electronic Resource
English
RESPONSE SURFACES FOR OPTIMAL WEIGHT OF CRACKED COMPOSITE PANELS: NOISE AND ACCURACY
British Library Conference Proceedings | 2000
|Residual strength of cracked stiffened panels
TIBKAT | 1971
|Residual Strength of Cracked Stiffened Panels
NTIS | 1967
|