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

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Bibliographic Details
Main Author Kroll, W. D.
Corporate Authors United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Format Electronic eBook
LanguageEnglish
Published Washington, D.C. : National Advisory Committee for Aeronautics, [1943]
SeriesWartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L398.
Subjects
Plates (Engineering)
Axial loads.
Loads (Mechanics)
Buckling (Mechanics)
Stability.
elektronické knihy
electronic books
Online AccessFull text
ISBN9781680156515
1680156519
Physical Description1 online resource (47 pages) : tables

Cover

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035 |a (OCoLC)914615508  |z (OCoLC)951660656 
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. 
506 |a Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty 
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. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Plates (Engineering) 
650 0 |a Axial loads. 
650 0 |a Loads (Mechanics) 
650 0 |a Buckling (Mechanics) 
650 0 |a Stability. 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
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://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpTSCFFRP2/tables-of-stiffness?kpromoter=marc  |y Full text 

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