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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) Buy on Amazon

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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)

AuthorGeorge W Lewis
PublisherFor sale by the National Technical Information Service]
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Book Details

Author(s)George W Lewis
PublisherFor sale by the National Technical Information Service]
ISBN / ASINB00072FK2E
ISBN-13978B00072FK23
MarketplaceIndia  🇮🇳

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