Optimum design of laminates with natural frequency constraints-Reference-Cited by-同舟云学术

Optimum design of laminates with natural frequency constraints

Published:1979-11 Issue:1 Volume:67 Page:101-112
ISSN:0022-460X
Container-title:Journal of Sound and Vibration
language:en
Short-container-title:Journal of Sound and Vibration

Author:

Rao S.S.,Singh K.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Acoustics and Ultrasonics,Condensed Matter Physics

Reference13 articles.

1. Advanced design concepts for advanced composite air frames;Foye;Air Force Materials Laboratory, Wright-Patterson Air Force Base, Ohio, AFML-TR-68-91,1968

2. Structural airframe application of advanced composite materials—analytical methods;Waddoups;Air Force Materials Laboratory, Wright-Patterson Air Force Base, Ohio, AFML-TR-69-101,1969

3. Structural synthesis of anisotropic plates;Waddoups,1970

4. Minimum weight design of stiffened fibre composite cylinders;Kicher;Journal of Aircraft,1971

5. Optimum laminate design for strength and stiffness;Schmit;International Journal for Numerical Methods in Engineering,1973

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