Deformation analysis of wing structures

The elementary theories of bending and torsion often do not describe the stresses in aircraft shell structures with adequate accuracy; more refined stress theories have therefore have developed over a period of years. Theories of this nature are applied to the problem of calculating the deflections,...

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Bibliographic Details
Main Author: Kuhn, Paul, (Author)
Corporate Author: Langley Aeronautical Laboratory.
Format: eBook
Language: English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1947.
Series: Technical note (United States. National Advisory Committee for Aeronautics) ; no. 1361.
Subjects:
Deformations (Mechanics)
Airplanes > Wings.
Strains and stresses.
Mathematics > Formulae.
elektronické knihy
electronic books
ISBN: 9781680156072
1680156071
Physical Description: 1 online resource (34 pages, 9 unnumbered pages) : illustrations

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Table of contents

LEADER 03004cam a2200457 i 4500
001 kn-ocn919093439
003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 150824s1947 dcua obt f000 0 eng d
040 |a KNOVL  |b eng  |e rda  |e pn  |c KNOVL  |d OCLCF  |d ZCU  |d OCLCQ  |d UAB  |d DKU  |d OCLCQ  |d CEF  |d RRP  |d WYU  |d YOU  |d AU@  |d OCL  |d S2H  |d OCLCO  |d COP  |d OCLCO  |d OCLCA  |d OCLCQ  |d UPM  |d OCLCQ  |d OCLCO  |d OCLCA  |d OCLCL 
020 |a 9781680156072  |q (electronic bk.) 
020 |a 1680156071  |q (electronic bk.) 
035 |a (OCoLC)919093439 
100 1 |a Kuhn, Paul,  |e author. 
245 1 0 |a Deformation analysis of wing structures /  |c by Paul Kuhn. 
264 1 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c 1947. 
300 |a 1 online resource (34 pages, 9 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 National Advisory Committee for Aeronautics technical note ;  |v number 1361 
500 |a "Langley Memorial Aeronautical Laboratory." 
500 |a Date of issue: July 1947. 
500 |a Report no. NACA TN No. 1361. 
504 |a Includes bibliographical references (page 34) 
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 elementary theories of bending and torsion often do not describe the stresses in aircraft shell structures with adequate accuracy; more refined stress theories have therefore have developed over a period of years. Theories of this nature are applied to the problem of calculating the deflections, particularly of wings. Bending as well as torsional deflections are discussed for wings without or with cut-outs. Whenever convenient, the formulas are given in such a form that they yield corrections to be added to the deflections calculated by means of the elementary theories. Examples show that the deflection corrections usually are quite small; very simple approximation formulas are therefore adequate for design purposes when conventional structures uder a reasonably uniform loading are being considered. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Deformations (Mechanics) 
650 0 |a Airplanes  |x Wings. 
650 0 |a Strains and stresses. 
650 0 |a Mathematics  |v Formulae. 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
710 1 |a United States.  |b National Advisory Committee for Aeronautics,  |e issuing body. 
710 2 |a Langley Aeronautical Laboratory. 
776 0 8 |i Print version:  |a Kuhn, Paul.  |t Deformation analysis of wing structures  |w (OCoLC)652863425 
830 0 |a Technical note (United States. National Advisory Committee for Aeronautics) ;  |v no. 1361. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpDAWSNAC1/deformation-analysis-of?kpromoter=marc  |y Full text 

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