The strength of shell bodies-- theory and practice

The monocoque form of airplane construction has introduced a number of new problems to the stress calculator and the designer. The problems for the stress calculator fall into two groups: the determination of the stress condition (shell statics) and the determination of the failing strength (shell s...

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Bibliographic Details
Main Author: Ebner, H., (Author)
Corporate Author: United States. National Advisory Commitee for Aeronautics.
Format: eBook
Language: English
Published: Washington, D.C. : National Advisory Commitee for Aeronautics, [1937]
Series: Technical memorandum (United States. National Advisory Committee for Aeronautics) ; no. 838.
Subjects:
Monocoque construction.
Shells (Engineering)
Strains and stresses.
Mathematics.
elektronické knihy
electronic books
ISBN: 9781680156560
168015656X
Physical Description: 1 online resource (51 pages, 9 unnumbered pages) : illustrations

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Table of contents

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001 kn-ocn919167954
003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 150825s1937 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 OCLCE  |d S2H  |d OCLCO  |d OCLCQ  |d UPM  |d OCLCQ  |d OCLCO  |d SXB 
020 |a 9781680156560  |q (electronic bk.) 
020 |a 168015656X  |q (electronic bk.) 
035 |a (OCoLC)919167954  |z (OCoLC)1111582255  |z (OCoLC)1117267102  |z (OCoLC)1229063301 
042 |a dlr 
100 1 |a Ebner, H.,  |e author. 
245 1 4 |a The strength of shell bodies-- theory and practice /  |c H. Ebner. 
264 1 |a Washington, D.C. :  |b National Advisory Commitee for Aeronautics,  |c [1937] 
300 |a 1 online resource (51 pages, 9 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 Technical memorandums ;  |v number 838 
500 |a "September 1937." 
500 |a NACA TM No. 838. 
500 |a Translated from Luftfahrtforschung. Vol. 14, No. 3, March 20, 1937, by the National Advisory Commitee for Aeronautics. 
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 The monocoque form of airplane construction has introduced a number of new problems to the stress calculator and the designer. The problems for the stress calculator fall into two groups: the determination of the stress condition (shell statics) and the determination of the failing strength (shell strength). The present report summarizes the most important theoretical and experimental results on this subject. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Monocoque construction. 
650 0 |a Shells (Engineering) 
650 0 |a Strains and stresses. 
650 0 |a Mathematics. 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
710 1 |a United States.  |b National Advisory Commitee for Aeronautics. 
776 0 8 |i Print version:  |a Ebner, H.  |t Strength of shell bodies - theory and practice  |w (OCoLC)696399361 
830 0 |a Technical memorandum (United States. National Advisory Committee for Aeronautics) ;  |v no. 838. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpSSBTPNA1/strength-of-shell?kpromoter=marc  |y Full text 

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