Development of Exit-Plane Probes for Turbine Engine Condition Monitoring-Reference-Cited by-同舟云学术

Development of Exit-Plane Probes for Turbine Engine Condition Monitoring

Published:2002-07-07 Issue: Volume: Page:
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Container-title:38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Hiers Robert,Hiers Robert

Publisher

American Institute of Aeronautics and Astronautics

Reference7 articles.

1. Jalbert,P.A.,andHiers,R.S.Jr."MachFlow Angularity Probes for Scramjet Engine Flow Path Diagnostics," SAE Paper Number 932551, Aerotech '93, Costa Mesa, California, 27 - 30September, 1993.

2. Hiers, R. S. Jr., and Hiers, R. S. III, "Development of High-Temperature Image Probes for Viewing Turbine Engine Augmentors." AIAA-2002-2912, 22ndAIAAAerodynamicMeasurementTechnology and Ground Testing Conference, St. Louis, Missouri, 24-27June 2002.

3. Hiers, R. S., and Pruitt, D. W. "Determination ofThrustfromPitotPressureMeasurements,"AIAA 2001-3314, 38thAIAA/ASME/SAE/ASEEJointPropulsion Conference and Exhibit, Salt Lake City, Utah, 8-11July 2001.

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