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 rat
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 rat” by George W…
Catalogue details
- Author
- George W. Lewis
- Category
- General & Other
- Language
- English
- Source
- HathiTrust