Inlet Distortion Test with Gas Turbine Engine in the Altitude Engine Test Facility-Reference-Cited by-同舟云学术

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Inlet Distortion Test with Gas Turbine Engine in the Altitude Engine Test Facility

Published:2010-06-28 Issue: Volume: Page:
ISSN:
Container-title:27th AIAA Aerodynamic Measurement Technology and Ground Testing Conference
language:
Short-container-title:

Author:

Lee Kyungjae¹,Lee Bohwa¹,Kang Sanghun¹,Yang Sooseok¹,Lee Daesung¹

Affiliation:

1. Korea Aerospace Research Institute

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-4337

Reference8 articles.

1. 1SAES-16Committee,ARP1420,"GasTurbineInletFlowDistortionGuidelines,"SocietyofAutomotiveEngineers,1978.

2. 3Yates,B.,andEagles,C."Engine3/23BGauzeandSwirlTest,"RollsRoyceLtd.,Bristol,1979.

3. 4Genbler,H.P.,Meyer,W.,andFottner,L."DevelopmentofIntakeSwirlGeneratorsforTurbojetEngineTesting,"AGARD CP-400, 1986.

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