A THEORETICAL SOLUTION FOR THE BUCKLING OF SANDWICH PANELS WITH LAMINATED FACE PLATES USING A COMPUTER ALGEBRA SYSTEM | 東京工業大学附属図書館文献データベース

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A THEORETICAL SOLUTION FOR THE BUCKLING OF SANDWICH PANELS WITH LAMINATED FACE PLATES USING A COMPUTER ALGEBRA SYSTEM

著者名:

掲載資料名:

NASA Technical Reports

発行年:

1989

通号:

N91-19486

ペーパー番号:

N91-19486

開始ページ:

1

終了ページ:

39

総ページ数:

39

出版情報:

National Aeronautics and Space Adminstration

言語:

英語

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:

ZA00001427

類似資料:

1 テクニカルペーパー AN EXPERT SYSTEM FOR LAMINATED PLATE DESIGN USING COMPOSITE MATERIALS Webber, J.P.H., Morton, S.K. National Aeronautics and Space Adminstration	7 テクニカルペーパー THEORETICAL INVESTIGATION OF STRESS CONCENTRATIONS IN DAMAGED CARBON FIBRE REINFORCED PLASTIC PLATE STRUCTURES. VOLUME 1: MAIN TEXT Final Report Webber, J. P.H. et al. National Aeronautics and Space Administration
2 テクニカルペーパー A KNOWLEDGE BASED EXPERT SYSTEM FOR LAMINATED COMPOSITE STRUT DESIGN WU. C.M.L., WEBBER, J.P.H., MORTON, S.K. National Aeronautics and Space Adminstration	8 テクニカルペーパー Vibration of Sandwich Panels Using {3,2}-Order Plate Theory H. Turkmen, V. Dogan, E. Madenci, A. Tessler American Institute of Aeronautics and Astronautics
3 テクニカルペーパー MINIMUM WEIGHT OPTIMIZATION OF COMPOSITE LAMINATED STRUTS WU, C.M.L., WEBBER, J.P.H. National Aeronautics and Space Adminstration	9 テクニカルペーパー The Buckling Response of Symmetrically Laminated Composite Plates Having a Trapezoidal Planform Area Radloff, H. D., II, Hyer, M. W., Nemeth, M. P. National Aeronautics and Space Adminstration
4 テクニカルペーパー Core and Face Sheet Anisotropy in Deformation and Buckling of Sandwich Panels Hohe, J., Librescu, L. American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Thermal buckling behavior in Al honeycomb sandwich plates with very thin CFRP faces Watanabe, Naoyuki, Sato, Hiroyuki, Nishi, Yasushi American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Global Buckling and Face Wrinkling Response of Sandwich Panels Under Transient Loads Hohe, J., Librescu, L., Oh, S. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Thermal Buckling of Metal Foam Sandwich Panels for Actively Cooled Thermal Protection Systems Rakow, J., Waas, A. American Institute of Aeronautics and Astronautics
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