NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Single-stage experimental evaluation of compressor blading with slots and vortex generators, part 5An experimental investigation was conducted to determine the extent that slots and vortex generators can increase the efficiency and stable operating range of highly loaded compressor stages. With slots in the rotor and stator, the stage performance both with and without vortex generators was inferior to that achieved with the unslotted blading. However, with vortex generators, stator slots, and an unslotted rotor, the stable operating range increased 25% and the stage peak efficiency increased 2.1% over the values achieved with the unslotted rotor and stator without vortex generators, at design equivalent rotor speed.
Document ID
19720015141
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Brent, J. A.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Date Acquired
September 2, 2013
Publication Date
March 31, 1972
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-72793
PWA-FR-4541-PT-5
Report Number: NASA-CR-72793
Report Number: PWA-FR-4541-PT-5
Accession Number
72N22791
Funding Number(s)
CONTRACT_GRANT: NAS3-10481
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available