Tensile properties of 7075-T6 and 2024-T3 aluminum-alloy sheet heated at uniform temperature rates under constant load

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Bibliographic Details
Main Author Heimerl, George J.
Corporate Author United States. National Advisory Committee for Aeronautics
Other Authors Inge, John E.
Format Electronic eBook
LanguageEnglish
Published Washington, D.C. : National Advisory Committee for Aeronautics, [1955]
SeriesTechnical note (United States. National Advisory Committee for Aeronautics) ; no. 3462.
Subjects
Aluminum alloys.
Plates (Engineering)
Loads (Mechanics)
Temperature.
Strains and stresses.
elektronické knihy
electronic books
Online AccessFull text
ISBN9781680156256
168015625X
Physical Description1 online resource (46 pages) : illustrations

Cover

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100 1 |a Heimerl, George J. 
245 1 0 |a Tensile properties of 7075-T6 and 2024-T3 aluminum-alloy sheet heated at uniform temperature rates under constant load /  |c George J. Heimerl and John E. Inge. 
264 1 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c [1955] 
300 |a 1 online resource (46 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 3462 
500 |a NACA TN No. 3462. 
504 |a Includes bibliographical references. 
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 Results are presented of tests to determine the effect of heating at uniform temperature rates from 0.2 degrees to 100 degrees F. per second on the tensile properties of 7075-T6 d(75s-T6) and 2024-T3 (24s-T3) aluminum-alloy sheet under constant-load conditions. Yield and rupture stresses, obtained under rapid-heating conditions, are compared with results of elevated-temperature stress-strain tests for 1/2-hour exposure. Master yield-and-rupture-stress curves based on linear temperature-rate parameter are presented with which yield and rupture stresses or temperatures may be predicted for these materials for temperature rates from 0.2 to 100 degrees F per second. A description of the test equipment is included. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Aluminum alloys. 
650 0 |a Plates (Engineering) 
650 0 |a Loads (Mechanics) 
650 0 |a Temperature. 
650 0 |a Strains and stresses. 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
700 1 |a Inge, John E. 
710 1 |a United States.  |b National Advisory Committee for Aeronautics. 
776 0 8 |i Print version:  |a Heimerl, George J.  |t Tensile properties of 7075-T6 and 2024-T3 aluminum-alloy sheet heated at uniform temperature rates under constant load  |w (OCoLC)680081595 
830 0 |a Technical note (United States. National Advisory Committee for Aeronautics) ;  |v no. 3462. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpTPTTAAS1/tensile-properties-of?kpromoter=marc  |y Full text 

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