|
|
|
|
LEADER |
00000cam a2200000 i 4500 |
001 |
KNOVEL_ocn914328247 |
003 |
OCoLC |
005 |
20231027140348.0 |
006 |
m o d f |
007 |
cr ||||||||||| |
008 |
150724s1952 ohua obt f000 0 eng d |
040 |
|
|
|a SINTU
|b eng
|e pn
|c SINTU
|d 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 TRAAL
|d OCLCQ
|d OCLCO
|
019 |
|
|
|a 951660471
|
020 |
|
|
|a 9781680156201
|q (electronic bk.)
|
020 |
|
|
|a 1680156209
|q (electronic bk.)
|
029 |
1 |
|
|a GBVCP
|b 856591580
|
035 |
|
|
|a (OCoLC)914328247
|z (OCoLC)951660471
|
050 |
|
4 |
|a TA660.P6
|
082 |
0 |
4 |
|a 624.17765
|2 23
|
086 |
0 |
|
|a Y 3.N 21/5:6/2661
|
088 |
|
|
|a NACA-TN-2661
|
049 |
|
|
|a UAMI
|
100 |
1 |
|
|a Kuhn, Paul.
|
245 |
1 |
2 |
|a A summary of diagonal tension.
|n Part 1,
|p Methods and analysis /
|c Paul Kuhn, James P. Peterson, and L. Ross Levin.
|
260 |
|
|
|a Washington, D.C. :
|b National Advisory Committee for Aeronautics,
|c 1952.
|
300 |
|
|
|a 1 online resource (131 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 National Advisory Committee for Aeronautics ;
|v no. 2661
|
500 |
|
|
|a "May 1952."
|
500 |
|
|
|a NACA TN No. 2661.
|
504 |
|
|
|a Includes bibliographical references.
|
520 |
3 |
|
|a Previously published methods for stress and strength analysis of plane and curved shear webs working in diagonal tension are presented as a unified method. The treatment is sufficiently comprehensive and detailed to make the paper self-contained. Part 1 discusses the theory and methods for calculating the stresses and shear deflections of web systems as well as the strengths of the web, the stiffeners, and the riveting. Part 2, published separately, presents the experimental evidence.
|
588 |
0 |
|
|a Print version record.
|
590 |
|
|
|a Knovel
|b ACADEMIC - Aerospace & Radar Technology
|
650 |
|
0 |
|a Plates (Engineering)
|
650 |
|
0 |
|a Bars (Engineering)
|
650 |
|
0 |
|a Strains and stresses.
|
650 |
|
0 |
|a Shear (Mechanics)
|
650 |
|
0 |
|a Mathematical analysis.
|
650 |
|
6 |
|a Plaques (Ingénierie)
|
650 |
|
6 |
|a Barres (Ingénierie)
|
650 |
|
6 |
|a Contraintes (Mécanique)
|
650 |
|
6 |
|a Cisaillement (Mécanique)
|
650 |
|
6 |
|a Analyse mathématique.
|
650 |
|
7 |
|a bars (building materials)
|2 aat
|
650 |
|
7 |
|a shear stress.
|2 aat
|
650 |
|
7 |
|a Bars (Engineering)
|2 fast
|
650 |
|
7 |
|a Mathematical analysis
|2 fast
|
650 |
|
7 |
|a Plates (Engineering)
|2 fast
|
650 |
|
7 |
|a Shear (Mechanics)
|2 fast
|
650 |
|
7 |
|a Strains and stresses
|2 fast
|
700 |
1 |
|
|a Peterson, James P.
|
700 |
1 |
|
|a Levin, L. Ross.
|
710 |
1 |
|
|a United States.
|b National Advisory Committee for Aeronautics.
|
730 |
0 |
|
|a Technical Report Archive & Image Library (TRAIL)
|
776 |
0 |
8 |
|i Print version:
|a Kuhn, Paul.
|t Summary of diagonal tension.
|d Washington, D.C. : National Advisory Committee for Aeronautics, 1952
|w (OCoLC)667213346
|
830 |
|
0 |
|a Technical note (United States. National Advisory Committee for Aeronautics) ;
|v no. 2661.
|
856 |
4 |
0 |
|u https://appknovel.uam.elogim.com/kn/resources/kpSDTPIMA1/toc
|z Texto completo
|
994 |
|
|
|a 92
|b IZTAP
|