Inlet distortion considerations for high cycle fatigue in gas turbine engine-Reference-Cited by-同舟云学术

Inlet distortion considerations for high cycle fatigue in gas turbine engine

Published:1997-07-06 Issue: Volume: Page:
ISSN:
Container-title:33rd Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Hamed Awatef¹,Numbers Keith²,Hamed Awatef¹,Numbers Keith²

Affiliation:

1. Cincinnati, Univ., OH

2. USAF, Research Lab., Wright-Patterson AFB, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-3364

Reference40 articles.

1. SAEAerospaceCouncilDivision Technical CommitteeS-16."InletTotal-Pressure-Distortion Considerations for Gas-TurbineEngines"SAE AerospaceInformation Report,AIR-1419,May 1983.

2. SAEAerospaceCouncilDivision Technical Committee S-16."GasTurbineEngineInletFlow Distortion Guidelines"SAEAerospaceInformation Report,ARP-1420,March, 1978.

3. Peacock,R.E.andOverli,J. "DynamicInternal Flows inCompressors with PressureMaldistributed InletConditions,"46thP.E.P.Conference ofAGARD, Monterey,CA,1975,pp.17-11- 17-12.

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