Charts for calculation of the critical compressive stress for local instability of idealized web- and T-stiffened panels

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Bibliographic Details
Main Author Boughan, Rolla B.
Corporate Authors United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Other Authors Baab, George W.
Format Electronic eBook
LanguageEnglish
Published Washington, D.C. : National Advisory Committee for Aeronautics, [1944]
SeriesWartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L204.
Subjects
Online AccessFull text
ISBN9781680156492
1680156497
Physical Description1 online resource (8, [6] pages) : illustrations

Cover

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020 |a 9781680156492  |q (electronic bk.) 
020 |a 1680156497  |q (electronic bk.) 
035 |a (OCoLC)914550863  |z (OCoLC)914551307  |z (OCoLC)951667263 
100 1 |a Boughan, Rolla B. 
245 1 0 |a Charts for calculation of the critical compressive stress for local instability of idealized web- and T-stiffened panels /  |c Rolla B. Boughan and George W. Baab. 
246 3 |a NACA Wartime Reports. Series L. 
260 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c [1944] 
300 |a 1 online resource (8, [6] 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 no. L204 
500 |a NACA Wartime Report L-204. 
500 |a Originally issued as NACA as Advance Restricted Report L4H29 (August 1944). 
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 Charts are presented for the calculation of the critical compressive stress - the stress at which local instability occurs - for idealized web- and T-stiffened panels, and examples of the use of the charts are given. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Aluminum alloys. 
650 0 |a Plates (Engineering) 
650 0 |a Strains and stresses. 
650 0 |a Buckling (Mechanics) 
650 0 |a Airplanes  |x Materials. 
650 0 |a Charts, diagrams, etc. 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
700 1 |a Baab, George W. 
710 1 |a United States.  |b National Advisory Committee for Aeronautics. 
710 2 |a Langley Aeronautical Laboratory. 
776 0 8 |i Print version:  |a Boughan, Rolla B.  |t Charts for calculation of the critical compressive stress for local instability of idealized web- and T-stiffened panels.  |d Washington, D.C. : National Advisory Committee for Aeronautics, [1944]  |w (OCoLC)706693060 
830 0 |a Wartime Reports (United States. National Advisory Committee for Aeronautics) ;  |v no. L204. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpCCCCSLI2/charts-for-calculation?kpromoter=marc  |y Full text