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

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 u...

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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: eBook
Language: English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1955]
Series: Technical 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
ISBN: 9781680156256
168015625X
Physical Description: 1 online resource (46 pages) : illustrations

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Table of contents

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001 kn-ocn919140856
003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 150825s1955 dcua obt f000 0 eng d
040 |a KNOVL  |b eng  |e rda  |e pn  |c KNOVL  |d ZCU  |d UAB  |d DKU  |d OCLCQ  |d CEF  |d RRP  |d YOU  |d S2H  |d OCLCO  |d OCLCQ  |d UPM  |d OCLCQ  |d TRAAL  |d GZM  |d OCLCO  |d OCLCL  |d SXB 
020 |a 9781680156256  |q (electronic bk.) 
020 |a 168015625X  |q (electronic bk.) 
035 |a (OCoLC)919140856  |z (OCoLC)1385367562 
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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