"Free Flexural Vibrations of Integrally-Stiffened and/or Stepped-Thickness Rectangular Plates or Panels with a Central Plate Stiffener"-Reference-Cited by-同舟云学术

"Free Flexural Vibrations of Integrally-Stiffened and/or Stepped-Thickness Rectangular Plates or Panels with a Central Plate Stiffener"

Published:2007-04-23 Issue: Volume: Page:
ISSN:
Container-title:48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
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Author:

Yuceoglu Umur¹,Gemalmayan Nihat²,Sunar Orkun²

Affiliation:

1. Middle East Tech University

2. Gazi University

Publisher

American Institute of Aeronautics and Astronautics

Link

Reference43 articles.

1. Hoskins, B.C. and Baker, A. A., 1986 "Composite Materials for Aircraft Structures", AIAA EducationalSeries, NewYork.

3. [3]Niu, M.C.Y. 1988,"AirframeStructuralDesign",CommilitPresLtd., Hong Kong.

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4. Free Vibrations Analysis of Integrally-Stiffened and/or Stepped-Thickness Plates or Panels with Two Side Stiffeners;49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference <br> 16th AIAA/ASME/AHS Adaptive Structures Conference<br> 10t;2008-04-07

5. Effects of Central and Non-Central Plate Stiffener on Free Vibrations Response of Integrally-Stiffened and/or Stepped-Thickness Plates or Panels;49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference <br> 16th AIAA/ASME/AHS Adaptive Structures Conference<br> 10t;2008-04-07