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