Residual strength and crack propagation tests on C-130 airplane center wings with service-imposed fatigue damage / H. Lawrence Snider, Franklin L. Reeder, and William Dirkin.
Fourteen C-130 airplane center wings, each containing service-imposed fatigue damage resulting from 4000 to 13,000 accumulated flight hours, were tested to determine their fatigue crack propagation and static residual strength characteristics. Eight wings were subjected to a two-step constant amplit...
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| Format: | Government Document Book |
| Language: | English |
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Washington, D.C. : Springfield, Va. :
National Aeronautics and Space Administration ; For sale by the National Technical Information Service [distributor],
1972.
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| Series: | NASA contractor report ;
NASA CR-2075. |
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Internet
Link to online resourceSearch for the full-text version of this title in HathiTrust
Norlin Library - Government Information - US
| Call Number: |
NAS 1.26:2075
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| NAS 1.26:2075 | Available Place a Hold |