Advances in Aerodynamic Probes for High-Enthalpy Applications-Reference-Cited by-同舟云学术

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Advances in Aerodynamic Probes for High-Enthalpy Applications

Published:2004-06-19 Issue: Volume: Page:
ISSN:
Container-title:24th AIAA Aerodynamic Measurement Technology and Ground Testing Conference
language:
Short-container-title:

Author:

MacKinnon Heather¹,Beitel Gregg¹,Hiers Robert¹,Catalano Daniel¹

Affiliation:

1. Aerospace Testing Alliance

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-2594

Reference11 articles.

1. Hiers, R. S. III, Beitel, G., and MacKinnon, H. "Development of Nozzle Exit Plane Probes for Rocket Applications - Status andPlans."NASAMSFC2003PropulsionMeasurementSensorDevelopmentWorkshop,May13-15,2003,Huntsville,Alabama.

2. Aerodynamics of Stream Thrust Probes

3. Design of Stream Thrust Probes in Reacting Flows

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2. Cooling of Miniature Flow-Field Probes for Combustion Measurements;42nd AIAA Thermophysics Conference;2011-06-14

3. Advanced Embedded Instrumentation for Gas Turbine Engines;2008 U.S. Air Force T&E Days;2008-02-05

4. Test Capabilities in the AEDC/UTSI J85 Turbojet Test Stand;2007 U.S. Air Force T&E Days;2007-02-13

5. Imaging Probes for Gas Turbine Engines;42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2006-07-09

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