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Bending of rectangular plates with large deflections /

The solution of Von Karman's fundamental equations for large deflections of plates is presented for the case of a simply supported rectangular plate under combined edge compression and lateral loading. Numerical solutions are given for square plates and for rectangular plates with a width-span...

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Levy, Samuel
Autor Corporativo: United States. National Advisory Committee for Aeronautics
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Washington, D.C. : G.P.O., 1942.
Colección:Report (United States. National Advisory Committee for Aeronautics) ; no. 737.
Temas:
Acceso en línea:Texto completo

MARC

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049 |a UAMI 
100 1 |a Levy, Samuel. 
245 1 0 |a Bending of rectangular plates with large deflections /  |c by Samuel Levy. 
260 |a Washington, D.C. :  |b G.P.O.,  |c 1942. 
300 |a 1 online resource (19 pages) 
336 |a text  |b txt  |2 rdacontent 
337 |a computer  |b c  |2 rdamedia 
338 |a online resource  |b cr  |2 rdacarrier 
490 1 |a Report / National Advisory Committee for Aeronautics ;  |v no. 737 
504 |a Includes bibliographical references. 
588 0 |a Print version record. 
520 |a The solution of Von Karman's fundamental equations for large deflections of plates is presented for the case of a simply supported rectangular plate under combined edge compression and lateral loading. Numerical solutions are given for square plates and for rectangular plates with a width-span ratio of 3:1. --  |c Provided by publisher. 
590 |a Knovel  |b ACADEMIC - Aerospace & Radar Technology 
650 0 |a Aeronautics  |x Research. 
650 0 |a Airplanes  |x Design and construction. 
650 6 |a Aéronautique  |x Recherche. 
650 6 |a Avions  |x Conception et construction. 
650 7 |a Aeronautics  |x Research  |2 fast 
650 7 |a Airplanes  |x Design and construction  |2 fast 
700 1 |a Levy, Samuel. 
710 1 |a United States.  |b National Advisory Committee for Aeronautics. 
776 0 8 |i Print version:  |a Levy, Samuel.  |t Bending of rectangular plates with large deflections.  |d Washington, D.C. : G.P.O., 1942  |w (OCoLC)46827401 
830 0 |a Report (United States. National Advisory Committee for Aeronautics) ;  |v no. 737. 
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994 |a 92  |b IZTAP