Nonlinear large-deflection boundary-value problems of rectangular plates

Relaxation and successive approximation methods are used to solve Von Karman's equations as applied to initially flat, rectangular plates with large deflections under either normal pressure or combined normal pressure and side thrust, and several specific cases are analyzed. The general method...

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Bibliographic Details
Main Author: Wang, Chi-Teh, (Author)
Format: eBook
Language: English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1948.
Series: Technical note (United States. National Advisory Committee for Aeronautics) ; no. 1425.
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ISBN: 9781680156096
1680156098
Physical Description: 1 online resource (113 pages) : illustrations, tables

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Summary: Relaxation and successive approximation methods are used to solve Von Karman's equations as applied to initially flat, rectangular plates with large deflections under either normal pressure or combined normal pressure and side thrust, and several specific cases are analyzed. The general method developed may be applied to bending and combined bending and buckling problems with practically any boundary conditions to any required degree of accuracy or applied to solve the membrane theory of the plate which applies when the deflection is very large in comparison with the thickness of the plate.
Item Description: Date of issue: March 1948.
Report no. NACA TN No. 1425.
Bibliography: Includes bibliographical references.
ISBN: 9781680156096
1680156098
Access: Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty