Cryogenic tunnel measurement of total temperature and pressure
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45296
Reference11 articles.
1. The application of cryogenics to high Reynolds number testing in wind tunnels. Part 1: Evolution, theory, and advantages
2. Lecture Series 42;Pindzola M.,1972
3. Noise Generation in Transonic Tunnels
4. Probe and method for simultaneous measurements of ’’true’’ instantaneous temperature and three velocity components in turbulent flow
5. Preliminary measurements of velocity, density and total temperature fluctuations in compressible subsonic flow
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1. Turbulence measurements and noise generation in a transonic cryogenic wind tunnel;AIAA Journal;1990-05
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