Design and experimental results for a turbine with jet flap stator and jet flap /
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- Created Date
Performing organization report no.: EDR 7389.
Includes bibliographical references (p. 44-45).
The overall performance and detailed stator performance of a negative hub reaction turbine design featuring a moderately low solidity jet flap stator and a jet flap rotor were determined. Testing was conducted over a range of turbine expansion ratios at design speed. At each expansion ratio, the stator jet flow and rotor jet flow ranged up to about 7 and 8 percent, respectively, of the turbine inlet flow. The performance of the jet flap stator/jet flap rotor turbine was compared with that of a turbine which used the same jet flap rotor and a conventional, high solidity plan stator. The effect on performance of increased axial spacing between the jet stator and rotor was also investigated.
Prepared by General Motors Corporation, Indianapolis, Ind. for Lewis Research Center
- Bettner, James L
- Contributing Institution
- University of Illinois
- Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor]
- Variable geometry structures
- Electronic resourceLanguage material
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- Chicago citation style
- Bettner, James L. Design and experimental results for a turbine with jet flap stator and jet flap /. 1973. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011431466. (Accessed September 23, 2018.)
- APA citation style
- Bettner, James L, (1973) Design and experimental results for a turbine with jet flap stator and jet flap /. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011431466
- MLA citation style
- Bettner, James L. Retrieved from the Digital Public Library of America <http://catalog.hathitrust.org/Record/011431466>.