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Design and cold-air investigation of a turbine for a small low-cost turbofan engine / by Milton G. Kofskey and William J. Nusbaum.
Connect to full text Available online
View online- Format:
- Book
- Government document
- Author/Creator:
- Kofskey, Milton G., author.
- Nusbaum, William J., author.
- Series:
- NASA technical note ; D-6967.
- NASA/TN ; D-6967
- Language:
- English
- Subjects (All):
- Airplanes--Turbofan engines.
- Airplanes.
- Axial flow compressors.
- Low temperatures.
- Gas-turbines--Testing.
- Physical Description:
- 1 online resource (31 pages) : illustrations.
- Place of Publication:
- Washington, D.C. : National Aeronautics and Space Administration, September 1972.
- Summary:
- An 8.00-in mean diameter two-stage turbine was investigated over a range of speeds from 0 to 110 percent of equivalent design speed and over a range of pressure ratios from 1.79 to 5.14. Presented are design information and turbine performance for first-stage and two-stage operation. Results are presented in terms of equivalent specific work, torque, mass flow, rotor exit flow angle, and efficiency.
- Notes:
- "September 1972."
- Includes bibliographical references (page 27).
- Description based on online resource, PDF version; title from title page (NASA, viewed on June 14, 2021).
- OCLC:
- 23014018
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