Dynamic contact analysis of laminated composite plates under low-velocity impact
- Author(s):
- Goo, Nam Seo ( Seoul National University, Korea )
- Kim, Seung Jo
- Jung, Sung Nam
- Publication title:
- A collection of technical papers : 37th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, April 15-17, 1996, Salt Lake City, UT
- Title of ser.:
- AIAA Paper : AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
- Ser. no.:
- CP962
- Pub. Year:
- 1996
- Vol.:
- pt. 2
- No.:
- 96-1405
- Paper no.:
- AIAA 96-1405
- Page(from):
- 776
- Page(to):
- 786
- Pub. info.:
- Washington, DC: American Institute of Aeronautics and Astronautics
- ISBN:
- 9781563472091 [1563472090]
- Language:
- English
- Call no.:
- A07400/962663(pt.1)A07400/962664,(pt.2)A07400/962665,(pt.3),A07400/962666(pt.4)
- Type:
- Technical Paper
Similar Items:
American Institute of Aeronautics and Astronautics |
7
Technical Paper
ANALYSES OF QUASI-ISOTROPIC COMPOSITE PLATES UNDER QUASI-STATIC POINT LOADS SIMULATING LOW-VELOCITY IMPACT
National Aeronautics and Space Administration |
2
Technical Paper
An explicit solution procedure of discontinuous time integration method for dynamic-contact/impact problems
American Institute of Aeronautics and Astronautics |
8
Technical Paper
Elasto-viscoplastic analysis of composite materials considering thermomechanical coupling effects
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
10
Technical Paper
THE EFFECT OF LOW VELOCITY IMPACT ON THE STRENGTH CHARACTERISTICS OF COMPOSITE MATERIALS LAMINATES Progress
National Aeronautics and Space Administration |
5
Technical Paper
Analysis of mindlin plate by the element free Galerkin method applying penalty technique
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
12
Technical Paper
DYNAMIC DELAMINATION BUCKLING IN COMPOSITE LAMINATES UNDER IMPACT LOADING: COMPUTATIONAL SIMULATION
National Aeronautics and Space Administration |