Gas Turbine Engine Flow-Field Diagnostics: Needs, Capabilities, and Proposed Development
Author:
Affiliation:
1. U.S. Air Force
2. Aerospace Testing Alliance
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-3440
Reference18 articles.
1. Development of Exit-Plane Probes for Turbine Engine Condition Monitoring
2. Advances in Aerodynamic Probes for High-Enthalpy Applications
3. Electroformed Diagnostic Probes for High-Temperature Gas Flows
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