Analytical and experimental study of flow through an axial turbine stage with a nonuniform inlet radial temperature profile-Reference-Cited by-同舟云学术

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Analytical and experimental study of flow through an axial turbine stage with a nonuniform inlet radial temperature profile

Published:1983-06-27 Issue: Volume: Page:
ISSN:
Container-title:19th Joint Propulsion Conference
language:
Short-container-title:

Author:

SCHWAB J.¹,STABE R.¹,WHITNEY W.¹

Affiliation:

1. NASA, Lewis Research Center, Cleveland, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1983-1175

Reference8 articles.

1. Calculation. ASME Paper 82-GT-239, Apr. 1982.

2. Core Turbine Facility and the Warm Annular Cascade Facility Recently Installed at NASA Lewis Research Center. NASA TM-81562, 1980.

3. Turbomachinery Performance. ASME Paper 74-GT-57, Mar. 1974. TABLE I. TURBINE TEST CONDITIONS

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