The strength and stiffness of shear webs with and without lightening holes

Nearly 200 tests were made on the strength of shear webs of 24S-T aluminum alloy, with and without lightening holes. The tests were made in a jig of the single-specimen type, in which the specimen is free to collapse completely without developing diagonal tension. The lightening holes were circular...

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Bibliographic Details
Main Author: Kuhn, Paul, (Author)
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, [1942]
Series: Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L402.
Subjects:
ISBN: 9781680156539
1680156535
Physical Description: 1 online resource (29 pages, 15 unnumbered pages) : illustrations

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Table of contents

LEADER 02836cam a2200505 i 4500
001 kn-ocn919163322
003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 150825s1942 dcua obt f000 0 eng d
040 |a KNOVL  |b eng  |e rda  |e pn  |c KNOVL  |d ZCU  |d OCLCQ  |d UAB  |d DKU  |d OCLCQ  |d CEF  |d RRP  |d YOU  |d S2H  |d OCLCO  |d OCLCQ  |d UPM  |d OCLCQ  |d OCLCO  |d OCLCL  |d SXB 
020 |a 9781680156539  |q (electronic bk.) 
020 |a 1680156535  |q (electronic bk.) 
035 |a (OCoLC)919163322 
100 1 |a Kuhn, Paul,  |e author. 
245 1 4 |a The strength and stiffness of shear webs with and without lightening holes /  |c Paul Kuhn. 
246 3 |a NACA Wartime Reports. Series L. 
264 1 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c [1942] 
300 |a 1 online resource (29 pages, 15 unnumbered pages) :  |b illustrations 
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 number L402 
500 |a NACA Wartime Report L-402. 
500 |a Originally issued as NACA as an Advance Restricted Report (June 1942). 
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 Nearly 200 tests were made on the strength of shear webs of 24S-T aluminum alloy, with and without lightening holes. The tests were made in a jig of the single-specimen type, in which the specimen is free to collapse completely without developing diagonal tension. The lightening holes were circular and had either flanged edges or beaded edges, the specimens with flanged edges constituting by far the largest test group. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Aluminum alloys. 
650 0 |a Holes. 
650 0 |a Shear (Mechanics) 
650 0 |a Strength of materials. 
650 0 |a Strains and stresses. 
650 0 |a Monocoque construction. 
650 0 |a Charts, diagrams, etc. 
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 Kuhn, Paul.  |t Strength and stiffness of shear webs with and without lightening holes  |w (OCoLC)707923695 
830 0 |a Wartime Reports (United States. National Advisory Committee for Aeronautics) ;  |v no. L402. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpSSSWLHND/strength-and-stiffness?kpromoter=marc  |y Full text