Experimental study of deformation and of effective width in axially loaded sheet-stringer panels

The deformation of two sheet-stringer panels subjected to end compression under carefully controlled end conditions was measured at a number of points and at a number of loads, most of which were above the load at which the sheet had begun to buckle. The two panels were identical except for the shee...

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Bibliographic Details
Main Authors: Ramberg, Walter, (Author), McPherson, Albert E., (Author), Levy, Sam, (Author)
Format: eBook
Language: English
Published: Washington [D.C.] : National Advisory Committee for Aeronautics, 1939.
Series: Technical note (United States. National Advisory Committee for Aeronautics) ; 684.
Subjects:
ISBN: 9781680156027
1680156020
Physical Description: 1 online resource (60 pages, 47 unnumbered pages) : illustrations

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001 kn-ocn913847994
003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 150716s1939 dcua ob f000 0 eng d
040 |a SINTU  |b eng  |e rda  |e pn  |c SINTU  |d SINTU  |d KNOVL  |d ZCU  |d OCLCQ  |d COD  |d OCLCF  |d OCLCQ  |d UAB  |d DKU  |d OCLCQ  |d CEF  |d RRP  |d YOU  |d TRAAL  |d GZM  |d COA  |d S2H  |d OCLCO  |d GPO  |d OCLCQ  |d OCLCO  |d OCLCQ  |d UPM  |d OCLCQ  |d OCLCO  |d OCLCL  |d SXB 
020 |a 9781680156027  |q (electronic bk.) 
020 |a 1680156020  |q (electronic bk.) 
035 |a (OCoLC)913847994  |z (OCoLC)951668819  |z (OCoLC)1154792931 
100 1 |a Ramberg, Walter,  |e author. 
245 1 0 |a Experimental study of deformation and of effective width in axially loaded sheet-stringer panels /  |c by Walter Ramberg, Albert E. McPherson, and Sam Levy. 
264 1 |a Washington [D.C.] :  |b National Advisory Committee for Aeronautics,  |c 1939. 
300 |a 1 online resource (60 pages, 47 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 note / National Advisory Committee for Aeronautics ;  |v No. 684 
500 |a "February 1939." 
500 |a No Federal Depository Library Program (FDLP) item number. 
504 |a Includes bibliographical references (pages 55-59). 
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 deformation of two sheet-stringer panels subjected to end compression under carefully controlled end conditions was measured at a number of points and at a number of loads, most of which were above the load at which the sheet had begun to buckle. The two panels were identical except for the sheet, which was 0.070-inch 24ST Alclad for specimen 1 and 0.25-inch 24ST aluminum alloy for specimen 6. A technique was developed for attaching Tuckerman optical strain gages to the sheeet by the method of attachment. This technique was used to explore the strain distribution in the sheet at various loads. The twisting and the bending of the stringers were measured by means of pointers attached to the stringers. The shape of the buckles in the sheet of specimen 6 was recorded at two loads by means of plaster casts. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Plates (Engineering) 
650 0 |a Aluminum alloys. 
650 0 |a Deformations (Mechanics) 
650 0 |a Buckling (Mechanics) 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
700 1 |a McPherson, Albert E.,  |e author. 
700 1 |a Levy, Sam,  |e author. 
710 1 |a United States.  |b National Advisory Committee for Aeronautics,  |e issuing body. 
776 0 8 |i Print version:  |a Ramberg, Walter.  |t Experimental study of deformation and of effective width in axially loaded sheet-stringer panels.  |d Washington D.C. : National Advisory Committee for Aeronautics ; 1939  |w (OCoLC)646048220 
830 0 |a Technical note (United States. National Advisory Committee for Aeronautics) ;  |v 684. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpESDEWAL2/experimental-study-of?kpromoter=marc  |y Full text