Determination of the blade-element performance of a small transonic rotor.

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Author
Hawkins, Wayne Randolph
Date
1976-12Advisor
Shreeve, Raymond P.
Metadata
Show full item recordAbstract
The blade-element performance of a small transonic
compressor rotor operating at high subsonic speeds is
reported. Measurements were made downstream using a small
calibrated pneumatic probe, with simultaneous measurements
of total pressure, velocity, turning angle, pitch angle,
and temperature. In addition, a program is presented to
calculate blade-element performance based on empirical data
contained in NASA SP-36.