Calculation of the 3-D viscous flow at the endwall leading edge region of an axial annular turbine cascade
By: Leonard Walitt ; prepared for National Aeronautics and Space Administration, Lewis Research Center under contract DAAK51-81-C-0047.
Contributors: Lewis Research Center.; Thermo Mechanical Systems Company.
Series: NASA contractor report -- 168275.; USAAVSCOM-TR -- 84-C-3.; AVSCOM technical report -- 84-C-3.; NASA contractor report -- NASA CR-168275.
Publisher: The Center
Published: 1984
Place of publication: [Cleveland, Ohio?
Language: eng
Format: Microform
Subjects: Turbomachines -- Fluid dynamics.
Other titles: Calculation of the three-D viscous flow at the endwall leading edge region of an axial annular turbine cascade.
Notes: "Thermo Mechanical System Company."

"August 1984."

"N84-31095"--Microfiche header.

Bibliography: p. 24-25.

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