Recommendations for numerical solution of reinforced-panel and fuselage-ring problems

Procedures are recommended for solving the equations of equilibrium of reinforced panels and isolated fuselage rings as represented by the external loads and the operations table established according to Southwell's method. From the solution of these equations the stress distribution can be eas...

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Bibliographic Details
Main Authors: Hoff, Nicholas J. 1906- (Author), Libby, Paul A., (Author)
Corporate Authors: United States. National Advisory Committee for Aeronautics., Polytechnic Institute of Brooklyn.
Format: eBook
Language: English
Published: Washington, D.C. : U.S. Government Printing Office, 1949.
Series: Report (United States. National Advisory Committee for Aeronautics) ; no. 934.
Subjects:
Aeronautics > Research.
Airplanes > Fuselage.
Airplanes > Design and construction.
elektronické knihy
electronic books
ISBN: 9781680156461
1680156462
Physical Description: 1 online resource (29 pages)

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Table of contents

LEADER 03009cam a2200421 i 4500
001 kn-ocn919161696
003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 150825s1949 dcu ob f000 0 eng d
040 |a KNOVL  |b eng  |e rda  |e pn  |c KNOVL  |d ZCU  |d TFW  |d UAB  |d DKU  |d OCLCQ  |d CEF  |d RRP  |d YOU  |d S2H  |d OCLCO  |d OCLCQ  |d UPM  |d OCLCQ  |d OCLCO  |d OCLCL  |d SXB  |d OCLCQ 
020 |a 9781680156461  |q (electronic bk.) 
020 |a 1680156462  |q (electronic bk.) 
035 |a (OCoLC)919161696 
100 1 |a Hoff, Nicholas J.  |q (Nicholas John),  |d 1906-  |e author.  |1 https://id.oclc.org/worldcat/entity/E39PBJcGkkvGg4pWQvqmmwtVG3 
245 1 0 |a Recommendations for numerical solution of reinforced-panel and fuselage-ring problems /  |c by N.J. Hoff and Paul A. Libby. 
264 1 |a Washington, D.C. :  |b U.S. Government Printing Office,  |c 1949. 
300 |a 1 online resource (29 pages) 
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 Report / National Advisory Committee for Aeronautics ;  |v number 934 
504 |a Includes bibliographical references (page 21). 
506 |a Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty 
520 |a Procedures are recommended for solving the equations of equilibrium of reinforced panels and isolated fuselage rings as represented by the external loads and the operations table established according to Southwell's method. From the solution of these equations the stress distribution can be easily determined. The method of systematic relaxations, the matrix-calculus method, and several other methods applicable in special cases are discussed. Definite recommendations are made for obtaining the solution of reinforced-panel problems which are generally designated as shear lag problems. The procedures recommended are demonstrated in the analysis of a number of panels. In the case of fuselage rings it is not possible to make definite recommendations for the solution of the equilibrium equations for all rings and loadings. --  |c Provided by publisher. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Aeronautics  |x Research. 
650 0 |a Airplanes  |x Fuselage. 
650 0 |a Airplanes  |x Design and construction. 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
700 1 |a Libby, Paul A.,  |e author. 
710 1 |a United States.  |b National Advisory Committee for Aeronautics. 
710 2 |a Polytechnic Institute of Brooklyn. 
776 0 8 |i Print version:  |a Hoff, N.J.  |t Recommendations for numerical solution of reinforced-panel and fuselage-ring problems  |w (OCoLC)46869359 
830 0 |a Report (United States. National Advisory Committee for Aeronautics) ;  |v no. 934. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpRNSRPFRJ/recommendations-for-numerical?kpromoter=marc  |y Full text 

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