Tensile properties and creep strength of three aluminum alloys exposed up to 25,000 hours at 200 ̊to 400 ̊F (370 ̊to 480 ̊K) /
| Main Authors: | , |
|---|---|
| Corporate Authors: | , |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. : Springfield, Va. :
National Aeronautics and Space Administration ; For sale by the Clearinghouse for Federal Scientific and Technical Information,
[1969]
Washington, D.C. : National Aeronautics and Space Administration, January 1969 |
| Series: | NASA technical note ;
D-5010 NASA technical note ; D-5010 |
| Subjects: |
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| 100 | 1 | |a Royster, Dick M | |
| 100 | 1 | |a Royster, Dick M., |e author |= ^A220294 | |
| 245 | 1 | 0 | |a Tensile properties and creep strength of three aluminum alloys exposed up to 25,000 hours at 200 ̊to 400 ̊F (370 ̊to 480 ̊K) / |c by Dick M. Royster |
| 260 | |a Washington, D.C. : |b National Aeronautics and Space Administration ; |a Springfield, Va. : |b For sale by the Clearinghouse for Federal Scientific and Technical Information, |c [1969] | ||
| 264 | 1 | |a Washington, D.C. : |b National Aeronautics and Space Administration, |c January 1969 | |
| 300 | |a 1 online resource (42 pages) : |b illustrations | ||
| 300 | |a 42 p. : |b ill. ; |c 27 cm | ||
| 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 NASA technical note, |x 0499-9339 ; |v NASA TN D-5010 | |
| 490 | 1 | |a NASA/TN ; |v D-5010 | |
| 500 | |a Prepared at Langley Research Center | ||
| 500 | |a This WorldCat-derived record is shareable under Open Data Commons ODC-BY, with attribution to OCLC |5 CTY | ||
| 500 | |a "January 1969." | ||
| 500 | |a "January 1969"--Cover | ||
| 504 | |a Includes bibliographical references (p. 12) | ||
| 504 | |a Includes bibliographical references (page 12) | ||
| 588 | |a Description based on online resource, PDF version; title from title page (NASA, viewed on May 12, 2021) | ||
| 590 | |a Copy 1 bound with D-5004 |c 8602086 (parent record's ckey) |b 36105024751625 (item id) | ||
| 596 | |a 22 | ||
| 596 | |a 31 | ||
| 650 | 0 | |a Aluminum alloys |x Creep | |
| 650 | 0 | |a Aluminum alloys |x Ductility | |
| 650 | 0 | |a Supersonic transport planes |x Materials |x Environmental testing | |
| 650 | 7 | |a Aluminum alloys |x Creep |2 fast |0 http://id.worldcat.org/fast/806316 | |
| 650 | 7 | |a Aluminum alloys |x Ductility |2 fast |0 http://id.worldcat.org/fast/806317 | |
| 650 | 7 | |a Tensile properties |2 nasat | |
| 710 | 1 | |a United States |b National Aeronautics and Space Administration |e issuing body. |= ^A80734 | |
| 710 | 1 | |a United States |b National Aeronautics and Space Administration. | |
| 710 | 2 | |a Langley Research Center | |
| 776 | 0 | 8 | |i Print version: |a Royster, Dick M |t Tensile properties and creep strength of three aluminum alloys exposed up to 25,000 hours at 200 ̊to 400 ̊F (370 ̊to 480 ̊K) |w (OCoLC)646012167 |
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