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

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.

Saved in:
Bibliographic Details
Main Author: Kroll, W. D.
Corporate Authors: United States. National Advisory Committee for Aeronautics., Langley Aeronautical Laboratory.
Format: eBook
Language: English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1943]
Series: Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L398.
Subjects:
Plates (Engineering)
Axial loads.
Loads (Mechanics)
Buckling (Mechanics)
Stability.
elektronické knihy
electronic books
ISBN: 9781680156515
1680156519
Physical Description: 1 online resource (47 pages) : tables

Cover

Table of contents

LEADER 02713cam a2200481 i 4500
001 kn-ocn914615508
003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 150728s1943 dcua obt f000 0 eng d
040 |a SINTU  |b eng  |e pn  |c SINTU  |d SINTU  |d KNOVL  |d ZCU  |d OCLCQ  |d UAB  |d DKU  |d OCLCQ  |d CEF  |d RRP  |d YOU  |d S2H  |d OCLCO  |d OCLCQ  |d OCLCO  |d OCLCQ  |d OCLCO  |d OCLCL  |d SXB  |d OCLCQ 
020 |a 9781680156515  |q (electronic bk.) 
020 |a 1680156519  |q (electronic bk.) 
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 

Similar Items