Performance of a high-work, low-aspect-ratio turbine tested with a realistic inlet radial temperature profile /

Bibliographic Details
Main Author:	Stabe, Roy G.
Corporate Author:	United States. National Aeronautics and Space Administration
Other Authors:	Whitney, Warren J., Moffitt, Thomas P.
Format:	Government Document Book
Language:	English
Published:	[Washington, D.C.] : [National Aeronautics and Space Administration], [1984]
Series:	NASA technical memorandum ; 83655.
Subjects:	Turbines > Testing. Axial flow. Low aspect ratio. Temperature profiles. Turbine blades. Turbine engines.
Online Access:	https://purl.fdlp.gov/GPO/LPS99490

Available Online