Home › Books › Overall and blade-element performance of a 1.20-pressure-ra…
Overall and blade-element performance of a 1.20-pressure-ratio fan stage at design blade setting angle (NASA technical memorandum) Buy on Amazon

https://www.ebooknetworking.net/books_detail-B00072DQLQ.html

Overall and blade-element performance of a 1.20-pressure-ratio fan stage at design blade setting angle (NASA technical memorandum)

AuthorGeorge W Lewis
PublisherFor sale by the National Technical Information Service]
Shop on Amazon — choose your country
🇺🇸 USA 🇨🇦 Canada 🇬🇧 UK 🇩🇪 Germany 🇫🇷 France 🇮🇳 India
Buy New on Amazon 🇨🇦

Book Details

Author(s)George W Lewis
PublisherFor sale by the National Technical Information Service]
ISBN / ASINB00072DQLQ
ISBN-13978B00072DQL9
MarketplaceCanada  🇨🇦

More Books by George W Lewis

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)
Effect of damper on overall and blade-element performa…
View
Donate to EbookNetworking
Prev
Next