Tables of stiffness and carry-over factor for flat rectangular plates under compression /

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Tables of stiffness and carry-over factor are presented for infinitely long flat plates subjected to a uniformly distributed longitudinal compressive load. The tables are intended for use in solving problems in the stability of structures composed of plates under compression.

Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Kroll, W. D.
Autores Corporativos: United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Washington, D.C. : National Advisory Committee for Aeronautics, [1943]
Colección:Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L398.
Temas:
Plates (Engineering)
Axial loads.
Loads (Mechanics)
Buckling (Mechanics)
Stability.
Plaques (Ingénierie)
Charges axiales.
Charges.
Flambage (Résistance des matériaux)
Stabilité.
axial loads.
warping.
buckling.
stability.
Axial loads
Stability
Acceso en línea:Texto completo

MARC

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082 0 4 |a 624.17765  |2 23 
049 |a UAMI 
100 1 |a Kroll, W. D. 
245 1 0 |a Tables of stiffness and carry-over factor for flat rectangular plates under compression /  |c W.D. Kroll. 
246 3 |a NACA Wartime Reports. Series L. 
260 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c [1943] 
300 |a 1 online resource (47 pages) :  |b tables 
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 Wartime Report / National Advisory Committee for Aeronautics ;  |v no. L398 
500 |a NACA Wartime Report L-398. 
500 |a Originally issued as NACA as Advance Restricted Report L3K27 (November 1943). 
500 |a Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia. 
504 |a Includes bibliographical references. 
520 3 |a Tables of stiffness and carry-over factor are presented for infinitely long flat plates subjected to a uniformly distributed longitudinal compressive load. The tables are intended for use in solving problems in the stability of structures composed of plates under compression. 
588 0 |a Print version record. 
590 |a Knovel  |b ACADEMIC - Aerospace & Radar Technology 
650 0 |a Plates (Engineering) 
650 0 |a Axial loads. 
650 0 |a Loads (Mechanics) 
650 0 |a Buckling (Mechanics) 
650 0 |a Stability. 
650 6 |a Plaques (Ingénierie) 
650 6 |a Charges axiales. 
650 6 |a Charges. 
650 6 |a Flambage (Résistance des matériaux) 
650 6 |a Stabilité. 
650 7 |a axial loads.  |2 aat 
650 7 |a warping.  |2 aat 
650 7 |a buckling.  |2 aat 
650 7 |a stability.  |2 aat 
650 7 |a Axial loads  |2 fast 
650 7 |a Buckling (Mechanics)  |2 fast 
650 7 |a Loads (Mechanics)  |2 fast 
650 7 |a Plates (Engineering)  |2 fast 
650 7 |a Stability  |2 fast 
710 1 |a United States.  |b National Advisory Committee for Aeronautics. 
710 2 |a Langley Aeronautical Laboratory. 
776 0 8 |i Print version:  |a Kroll, W.D.  |t Tables of stiffness and carry-over factor for flat rectangular plates under compression.  |d Washington, D.C. : National Advisory Committee for Aeronautics, [1943]  |w (OCoLC)707742892 
830 0 |a Wartime Reports (United States. National Advisory Committee for Aeronautics) ;  |v no. L398. 
856 4 0 |u https://appknovel.uam.elogim.com/kn/resources/kpTSCFFRP2/toc  |z Texto completo 
994 |a 92  |b IZTAP 

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