Investigation of a 10-stage subsonic axial-flow research compressor 3: investigation of rotating stall, blade vibration and surge at low and intermediate compressor speeds Metadata
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- Main Title Investigation of a 10-stage subsonic axial-flow research compressor 3: investigation of rotating stall, blade vibration and surge at low and intermediate compressor speeds
- Series Title NACA Research Memorandums
Author: Huppert, Merle C.Creator Type: Personal
Author: Costilow, Eleanor L.Creator Type: Personal
Author: Budinger, Ray E.Creator Type: Personal
Originator: Lewis Flight Propulsion LaboratoryContributor Type: OrganizationContributor Info: National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab
- Creation: 1953-05-18
- Content Description: Report presenting an investigation of rotating stall and surge at low and intermediate speeds conducted on a 10-stage subsonic axial-flow research compressor. Fluctuations of rotating stall and surge were detected by hot-wire anemometers and pressure transducers. Results regarding overall performance and rotating stall, rotating stall and blade vibration, surge, and discussion of surge are provided.
- Physical Description: 40 p. : ill.
- Keyword: aircraft compressors
- Keyword: stall characteristics
Name: National Advisory Committee for Aeronautics CollectionCode: NACA
Name: Technical Report Archive and Image LibraryCode: TRAIL
Name: UNT Libraries Government Documents DepartmentCode: UNTGD
- Rights Access: public
- Rights License: pd
- Rights Statement: No Copyright, Unclassified, Unlimited, Publicly available
- Accession or Local Control No: 93R17095
- URL: http://hdl.handle.net/2060/19930087805
- Report No.: NACA-RM-E53C19
- Center for AeroSpace Information Number: 19930087805
- Archival Resource Key: ark:/67531/metadc59783
- Display Note: "III."