Current Airframe Propulsion Integration Testing Techniques at AEDC-Reference-Cited by-同舟云学术

Current Airframe Propulsion Integration Testing Techniques at AEDC

Published:2004-06-21 Issue: Volume: Page:
ISSN:
Container-title:USAF Developmental Test and Evaluation Summit
language:
Short-container-title:

Author:

Smith Charles¹,Bergmann Judy¹,Riddle Terry¹

Affiliation:

1. Arnold Engineering Development Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-6819

Reference13 articles.

1. "Inlet Total-Pressure-Distortion Considerations for Gas-Turbine Engines," AIR 1419, Rev. A, issued by SAE S-16 Turbine Engine Inlet FlowDistortionCommittee, March1999.

2. Lucas, E. J. "Evaluation of Wind Tunnel Nozzle Afterbody Test Techniques Utilizing a Modern Twin Engine Fighter Geometryat MachNumbers from0.6 to 1.2," AEDC-TR-79-63 (AD-A091545),October1980.

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