Application of a quasi-3D inviscid flow and boundary layer analysis to the hub-shroud contouring of a radial turbine
By: Kestutis C. Civinskas and Louis A. Povinelli.
Contributors: Povinelli, Louis A.; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 83669.; USAAVSCOM technical report -- 84-C-1.; AVSCOM technical report -- 84-C-1.
Publisher: National Aeronautics and Space Administration
Published: 1984
Place of publication: [Washington, D.C.?
Language: eng
Format: Microform
Subjects: Boundary layer.; Turbines -- Aerodynamics.
Notes: "N84-25647"--Microfiche header.

"AIAA-84-1297."

Includes bibliographical references.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration, 1984]. 1 microfiche ; 11 x 15 cm.