عرض للأخصائي: Overall and blade element performance of a 1.20 pressure ratio fan stage with rotor blades reset -7 ̊ / George W. Lewis and George Kovich ; Lewis Research Center, Cleveland, Ohio.

Summary goes here

محفوظ في:

التفاصيل البيبلوغرافية
التنسيق:	كتاب
اللغة:	الإنجليزية
الموضوعات:	Compressors Performance tests. Rotor blades (Turbomachinery) Turbofans. Axial flow. Engine design. Short haul aircraft. Turbocompressors.
الوسوم:	إضافة وسم لا توجد وسوم, كن أول من يضع وسما على هذه التسجيلة!

era
format	Book
genre
geographic
id	3b4bdda6-da58-4e1a-9ba5-bf775fbdbf8c
isbn
issn
language	eng
physical	[1], 80 pages :illustrations ;27 cm
publication	– publisher: US National Aeronautics and Space Administration dateOfPublication: 1976
publishDate	1976
subjects
title	Overall and blade element performance of a 1.20 pressure ratio fan stage with rotor blades reset -7 ̊ / George W. Lewis and George Kovich ; Lewis Research Center, Cleveland, Ohio.
topic	Compressors Compressors Performance tests. Rotor blades (Turbomachinery) Turbofans. Axial flow. Engine design. Short haul aircraft. Turbocompressors.