An experimental study of fatigue crack growth in aluminum sheet subjected to combined bending and membrane stresses /
| Main Author: | |
|---|---|
| Corporate Author: | |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Hampton, Va. : [Springfield, Va. :
National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor,
1997]
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], [1997] |
| Series: | NASA technical memorandum ;
4784 NASA technical memorandum 4784 |
| Subjects: |
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| 100 | 1 | |a Phillips, Edward P | |
| 245 | 1 | 3 | |a An experimental study of fatigue crack growth in aluminum sheet subjected to combined bending and membrane stresses / |c Edward P. Phillips |
| 260 | |a Hampton, Va. : |b National Aeronautics and Space Administration, Langley Research Center ; |a [Springfield, Va. : |b National Technical Information Service, distributor, |c 1997] | ||
| 260 | |a Hampton, Va. : |b National Aeronautics and Space Administration, Langley Research Center ; |a [Springfield, Va.] : |b [National Technical Information Service, distributor], |c [1997] | ||
| 300 | |a 1 v | ||
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| 490 | 1 | |a NASA technical memorandum ; |v 4784 | |
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| 533 | |a Microfiche |b [Washington, D.C. : |c National Aeronautics and Space Administration, |d 1997] |e 1 microfiche. | ||
| 533 | |a Microfiche |b [Washington, D.C. : |c National Aeronautics and Space Administration, |d 1997]. |e 1 microfiche. | ||
| 596 | |a 1 | ||
| 650 | 0 | |a Aluminum alloys | |
| 650 | 0 | |a Aluminum | |
| 650 | 0 | |a Metals |x Fatigue | |
| 650 | 7 | |a Aluminum alloys |2 fast | |
| 650 | 7 | |a Aluminum alloys |2 nasat | |
| 650 | 7 | |a Aluminum |2 fast | |
| 650 | 7 | |a Aluminum |2 nasat | |
| 650 | 7 | |a Bending fatigue |2 nasat | |
| 650 | 7 | |a Combined stress |2 nasat | |
| 650 | 7 | |a Crack propagation |2 nasat | |
| 650 | 7 | |a Fatigue (Materials) |2 nasat | |
| 650 | 7 | |a Metal sheets |2 nasat | |
| 650 | 7 | |a Metals |x Fatigue |2 fast | |
| 650 | 7 | |a Stress ratio |2 nasat | |
| 710 | 2 | |a Langley Research Center | |
| 776 | 0 | 8 | |i Online version: |a Phillips, Edward P |t Experimental study of fatigue crack growth in aluminum sheet subjected to combined bending and membrane stresses |w (OCoLC)945556941 |
| 776 | 0 | 8 | |i Print version: |t Experimental study of fatigue crack growth in aluminum sheet subjected to combined bending and membrane stresses ... nasa-tm-4784 ... nov. 7, 1997 |w (OCoLC)213891493 |
| 830 | 0 | |a NASA technical memorandum ; |v 4784 | |
| 830 | 0 | |a NASA technical memorandum |v 4784 | |
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