Mixer-Ejector Wall Pressure and Temperature Measurements Based on Photoluminescence
Author:
Affiliation:
1. University of Kansas, Lawrence, Kansas 66045
2. Illinois Institute of Technology, Chicago, Illinois 60616-3793
3. NASA John H. Glenn Research Center at Lewis Field, Cleveland, Ohio 44135
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1707
Reference20 articles.
1. Flow Characteristics of a Rectangular Multielement Supersonic Mixer-Ejector
2. AEROACOUSTIC CHARACTERISTICS OF A RECTANGULAR MULTI-ELEMENT SUPERSONIC JET MIXER–EJECTOR NOZZLE
3. Luminescent barometry in wind tunnels
4. Aerodynamic measurements based on photoluminescence
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