Wall Shear and Boundary-Layer Measurements in Shock Seperated Flow
Author:
Affiliation:
1. The Johns Hopkins University, Silver Spring, Md.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference14 articles.
1. X‐Band Measurement of Shock‐Tube Plasma Temperature
2. Attempted Microwave Measurement of Temperature of a Shock-Heated Plasma
3. Measurement of Plasma Temperature Using a Waveguide Probe
4. Determination of electron temperature of shock-heated plasma from microwave measurements
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