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DESIGN AND EXPERIMENTAL INVESTIGATION OF A SINGLE-STAGE TURBINE WITH A ROTOR ENTERING RELATIVE MACH NUMBER OF 2

By Moffitt, T. P

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Book Id: WPLBN0002196792
Format Type: PDF eBook :
File Size:
Reproduction Date: 2012

Title: DESIGN AND EXPERIMENTAL INVESTIGATION OF A SINGLE-STAGE TURBINE WITH A ROTOR ENTERING RELATIVE MACH NUMBER OF 2  
Author: Moffitt, T. P
Volume:
Language: English
Subject: PERFORMANCE, ROTOR SPEED, PERFORMANCE CHARACTERISTICS
Collections: NASA Publication Collection
Historic
Publication Date:
21443
Publisher:

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P, M. T. (21443). DESIGN AND EXPERIMENTAL INVESTIGATION OF A SINGLE-STAGE TURBINE WITH A ROTOR ENTERING RELATIVE MACH NUMBER OF 2. Retrieved from http://www.worldlibrary.in/


Description
Supplemental catalog subcollection information: NASA Publication Collection; Astrophysics and Technical Documents; Design of single-stage turbine for rotor entering at supersonic speed - performance characteristics

Summary
Contributor: National Aeronautics and Space Administration (NASA). The digitalization of this book was sponsored by National Aeronautics and Space Administration (NASA); Additional Subject Descriptions: PERFORMANCE; ROTOR SPEED; PERFORMANCE CHARACTERISTICS; TURBINES; ROTORS; SUPERSONIC SPEED; ROTOR; TURBINE

 

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