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)

Name: 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)
Author: George W Lewis
ISBN: 978B00072FK23

Author George W Lewis

Publisher For sale by the National Technical Information Service]

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Book Details

Author(s) George W Lewis

Publisher For sale by the National Technical Information Service]

ISBN / ASIN B00072FK2E

ISBN-13 978B00072FK23

Marketplace United States 🇺🇸

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)

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