Handbook of structural stability. Part 5, Compressive strength of flat stiffened panels /

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Bibliographic Details
Main Author Gerard, George
Corporate Author United States. National Advisory Committee for Aeronautics
Other Authors Becker, Herbert, 1918-
Format Electronic eBook
LanguageEnglish
Published Washington, D.C. : National Advisory Committee for Aeronautics, [1957]
SeriesTechnical note (United States. National Advisory Committee for Aeronautics) ; no. 3785.
Subjects
Online AccessFull text
ISBN9781680156300
1680156306
Physical Description1 online resource (ii, 89 pages) : illustrations

Cover

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100 1 |a Gerard, George. 
245 1 0 |a Handbook of structural stability.  |n Part 5,  |p Compressive strength of flat stiffened panels /  |c George Gerard. 
260 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c [1957] 
300 |a 1 online resource (ii, 89 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 note / National Advisory Committee for Aeronautics ;  |v 3785 
500 |a NACA TN No. 3785. 
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 A generalized crippling analysis for short monolithic panels with formed or extruded stiffeners is presented. The analysis applies to monolithic panels. Criteria are given for rivete panels which indicate if the panels can be considered to behave in a monolithic manner. Riveted panels that are subject to interrivet buckling and wrinkling or forced crippling do not behave in this manner. Methods are presented for estimating the strength of such panels. 
520 3 |a Intermediate-length and long stiffened panels are subject to other failure modes. Methods are given for estimating the column strength of panels. Various forms of column curves and direct-reading charts are considered. Theory and test data on optimum stiffened panels are presented for use in preliminary design studies. 
520 3 |a In box types of construction, the rib and spar structures influence the compressive strength of the stiffened panel. The various factors which can be of importance are considered. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Structural analysis (Engineering) 
650 0 |a Stability. 
650 0 |a Plates (Engineering) 
650 0 |a Materials  |x Compression testing. 
650 0 |a Buckling (Mechanics) 
650 0 |a Loads (Mechanics) 
650 0 |a Strains and stresses. 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
700 1 |a Becker, Herbert,  |d 1918-  |1 https://id.oclc.org/worldcat/entity/E39PCjBkyVMVhr9C9DTVXK7Hvd 
710 1 |a United States.  |b National Advisory Committee for Aeronautics. 
776 0 8 |i Print version:  |a Gerard, George.  |t Handbook of structural stability.  |d Washington, D.C. : National Advisory Committee for Aeronautics, [1957]  |w (OCoLC)682901595 
830 0 |a Technical note (United States. National Advisory Committee for Aeronautics) ;  |v no. 3785. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpHSSPVCS3/handbook-of-structural?kpromoter=marc  |y Full text