The influence of impact velocity on the tensile characteristics of some aircraft metals and alloys /

This report deals principally with the results of tension tests on sixteen metals and alloys, most of which are employed extensively in aircraft construction. The tension characteristics are discussed for static conditions and rates of deformation up to about 150 feed per second.

Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Clark, Donald S. (Donald Sherman) (Autor)
Formato: Documento de Gobierno Electrónico eBook
Idioma:Inglés
Publicado: Washington, [D.C.] : National Advisory Committee for Aeronautics, 1942.
Colección:Technical note (United States. National Advisory Committee for Aeronautics) ; 868.
Temas:
Airplanes > Materials > Testing.
Aeronautics > Research.
Aéronautique > Recherche.
Acceso en línea:Texto completo

MARC

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008 150728s1942 dcua ob f000 0 eng c
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019 |a 951670195  |a 1164733697 
020 |a 9781680156324  |q (electronic bk.) 
020 |a 1680156322  |q (electronic bk.) 
029 1 |a GBVCP  |b 856591785 
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050 4 |a TL698 
082 0 4 |a 629.134  |2 23 
086 0 |a Y 3.N 21/5:6/868 
049 |a UAMI 
100 1 |a Clark, Donald S.  |q (Donald Sherman),  |e author. 
245 1 4 |a The influence of impact velocity on the tensile characteristics of some aircraft metals and alloys /  |c by Donald S. Clark. 
264 1 |a Washington, [D.C.] :  |b National Advisory Committee for Aeronautics,  |c 1942. 
300 |a 1 online resource (34 pages, 28 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. 868 
588 |a Description based on online resource, PDF version; title from title page (TRAIL, viewed May 13, 2022). 
500 |a "October 1942." 
500 |a No Federal Depository Library Program (FDLP) item number. 
504 |a Includes bibliographical references (page 22). 
520 3 |a This report deals principally with the results of tension tests on sixteen metals and alloys, most of which are employed extensively in aircraft construction. The tension characteristics are discussed for static conditions and rates of deformation up to about 150 feed per second. 
520 3 |a As a result of these tests, it has been shown that Dowmetal M and 18-percent chromium - 8 percent nickel stainless steel are adversely affected by an increasing rate of deformation. The other materials tested exhibit changes in yield stress, ultimate strength, and other tensile properties. 
583 1 |a digitized  |c 2011  |h University of North Texas  |l committed to preserve  |2 pda  |5 TXdn. 
590 |a Knovel  |b ACADEMIC - Aerospace & Radar Technology 
650 0 |a Airplanes  |x Materials  |x Testing. 
650 0 |a Aeronautics  |x Research. 
650 6 |a Aéronautique  |x Recherche. 
650 7 |a Aeronautics  |x Research.  |2 fast  |0 (OCoLC)fst00798376 
650 7 |a Airplanes  |x Materials  |x Testing.  |2 fast  |0 (OCoLC)fst00803297 
710 1 |a United States.  |b National Advisory Committee for Aeronautics,  |e issuing body. 
776 0 8 |i Print version:  |a Clark, Donald S. (Donald Sherman).  |t Influence of impact velocity on the tensile characteristics of some aircraft metals and alloys.  |d Washington, D.C. : National Advisory Committee for Aeronautics, 1942  |w (OCoLC)53947118 
830 0 |a Technical note (United States. National Advisory Committee for Aeronautics) ;  |v 868. 
856 4 0 |u https://appknovel.uam.elogim.com/kn/resources/kpIIVTCSA1/toc  |z Texto completo 
994 |a 92  |b IZTAP 

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