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George W Lewis
Books by George W Lewis
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Overall and blade-element performance of a 1.20-pressure-ratio fan stage at design blade setting angle (NASA technical memorandum)
George W Lewis
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Effect of damper on overall and blade-element performance of a compressor rotor having a tip speed of 1151 feet per second and an aspect ratio of 3.6 (NASA technical memorandum)
George W Lewis
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