Effects of interstage diffuser flow distortion on the performance of a 15.41- centimeter tip diameter axial power turbine [microform] / Kerry L. McLallin, Milton G, Kofskey, and Kestutis C. Civinskas ; work performed for U.S. Department of Energy ; prepared for Nineteenth Joint Propulsion Conference by the AIAA, SAE, and ASME Seattle, Washington, June 27-29, 1983.

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Bibliographic Details
Main Author:	McLallin, Kerry L.
Corporate Authors:	Lewis Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Society of Automotive Engineers, United States. Department of Energy, United States. Army Aviation Research and Development Command, American Institute of Aeronautics and Astronautics, Army Research and Technology Laboratories (U.S.), American Society of Mechanical Engineers, Joint Propulsion Conference and Exhibit
Other Authors:	Kofskey, Milton G. (Originator), Civinskas, Kestutis C.
Format:	Government Document Conference Proceeding Book
Language:	English
Published:	[Washington, D.C.] : [National Aeronautics and Space Administration, 1983]
Series:	AVRADCOM technical report ; 83-C-2 NASA technical memorandum ; 83359. AIAA ; 83-1179.
Subjects:	Turbines > Aerodynamics. Axial flow turbines > Aerodynamics. Performance (Engineering) Turbine stators.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.15:83359
NAS 1.15:83359	Restricted Place a Hold