2 options
Cold-air investigation of effects of partial admission on performance of 3.75-inch mean-diameter single-stage axial-flow turbine / by Hugh A. Klassen.
- Format:
- Book
- Government document
- Author/Creator:
- Klassen, Hugh A., author.
- Series:
- NASA technical note ; D-4700.
- NASA technical note ; TN D-4700
- Language:
- English
- Subjects (All):
- Turbines--Blades--Testing.
- Turbines.
- Turbines--Design and construction.
- Physical Description:
- 1 online resource (19 pages) : illustrations.
- Place of Publication:
- Washington, D.C. : National Aeronautics and Space Administration, August 1968.
- Notes:
- "August 1968."
- Includes bibliographical references (page 19).
- Description based on online resource, PDF version; title from title page (NASA, viewed on Dec. 4, 2020).
- Electronic reproduction. [Place of publication not identified]: HathiTrust Digital Library. 2024.
- Other Format:
- Print version: Klassen, Hugh A. Cold-air investigation of effects of partial admission on performance of 3.75-inch mean-diameter single-stage axial-flow turbine.
- OCLC:
- 761188102
- Access Restriction:
- Use copy Restrictions unspecified
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