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

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.

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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: eBook
Language: English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1944]
Series: Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L204.
Subjects:
Aluminum alloys.
Plates (Engineering)
Strains and stresses.
Buckling (Mechanics)
Airplanes > Materials.
Charts, diagrams, etc.
elektronické knihy
electronic books
ISBN: 9781680156492
1680156497
Physical Description: 1 online resource (8, [6] pages) : illustrations

Cover

Table of contents

LEADER 02861cam a2200505 a 4500
001 kn-ocn914550863
003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 150727s1944 dcua obt f000 0 eng d
040 |a SINTU  |b eng  |e pn  |c 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 
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 

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