Thermal buckling behavior in Al honeycomb sandwich plates with very thin CFRP faces

Thermal buckling behavior in Al honeycomb sandwich plates with very thin CFRP faces

Author(s):

Watanabe, Naoyuki ( Tokyo Metropolitan Institute of Technology, Tokyo, JAPAN )
Sato, Hiroyuki ( Tokyo Metropolitan Institute of Technology, Tokyo, JAPAN )
Nishi, Yasushi ( Tokyo Metropolitan Institute of Technology, Tokyo, JAPAN )

Publication title:

A collection of technical papers : 38th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit and AIAA/ASME/AHS Adaptive Structures Forum, April 7-10, 1997, Kissimmee, FL

Title of ser.:

AIAA Paper : AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference

Ser. no.:

CP973

Pub. Year:

1997

Vol.:

pt. 4

No.:

97-1249

Paper no.:

AIAA-97-1249

Page(from):

2492

Page(to):

2501

Pub. info.:

Reston, Va: American Institute of Aeronautics and Astronautics

ISBN:

9781563472275 [1563472279]

Language:

English

Call no.:

(pt.1)A07400/970595,(pt.2)A07400/970596,(pt.3)A07400/970597,(pt.4)A07400/970598

Type:

Technical Paper

Details

TDL ID:	ZA00006871
Series ID:	PA00000154
Conf. info. (Name):	AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit and AIAA/ASME/AHS Adaptive Structures Forum
Conf. info. (Number):	38th
Conf. info. (Venue):	Kissimmee, FL
Conf. info. (Date):	1997.04.07-1997.04.10

Similar Items:

1 Technical Paper Thermal Behavior of a Titanium Honeycomb-Core Sandwich Panel Ko, William L., Jackson, Raymond H. National Aeronautics and Space Adminstration	7 Technical Paper Thermal characterization of honeycomb sandwich structures Copenhaver, David C., Scott, Elaine P., Hanuska, Alexander American Institute of Aeronautics and Astronautics
2 Technical Paper Effect of Non-Uniform Core on Buckling and Post-Buckling Behavior of Sandwich Plates Lee, K., Lee, S., Jeon, S. American Institute of Aeronautics and Astronautics	8 Technical Paper Vibration analysis of multiple plates interacting with air Watanabe, Naoyuki, Tanzawa, Yasuyo, Narahashi, Hidehiko American Institute of Aeronautics and Astronautics
3 Technical Paper A THEORETICAL SOLUTION FOR THE BUCKLING OF SANDWICH PANELS WITH LAMINATED FACE PLATES USING A COMPUTER ALGEBRA SYSTEM Webber, J.P.H., Stewart, I.B. National Aeronautics and Space Adminstration	9 Technical Paper Combined-Load Buckling Behavior of MEtal-Matrix Composite Sandwich Panels Under Different Thermal Environments Ko, William L., Jackson, Raymond H. National Aeronautics and Space Adminstration
4 Technical Paper Buckling Behavior of Long Anisotropic Plates Subjected to Fully Restrained Thermal Expansion Nemeth,M. American Institute of Aeronautics and Astronautics	10 Technical Paper Buckling behavior of long anisotropic plates subjected to restrained thermal expansion and mechanical loads Nemeth, Michael P. American Institute of Aeronautics and Astronautics
5 Technical Paper Buckling Behavior of Long Anisotropic Plates Subjected to Elastically Restrained Thermal Expansion Nemeth, M. American Institute of Aeronautics and Astronautics	11 Technical Paper Global Buckling and Face Wrinkling Response of Sandwich Panels Under Transient Loads Hohe, J., Librescu, L., Oh, S. American Institute of Aeronautics and Astronautics
6 Technical Paper Mechanical- and Thermal-Buckling Behavior of Rectangular Plates With Different Central Cutouts Ko, William L. National Aeronautics and Space Adminstration	12 Technical Paper Core and Face Sheet Anisotropy in Deformation and Buckling of Sandwich Panels Hohe, J., Librescu, L. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12