Computing Measured Spectra from Hypersonic Pitot Probes with Flow-Parallel Freestream Disturbances
Author:
Affiliation:
1. University of Minnesota, Minneapolis, Minnesota 55455
Funder
Air Force Office of Scientific Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.J055396
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4. SteenL. E. “Characterization and Development of Nozzles for a Hypersonic Quiet Wind Tunnel,” M.S. Thesis, School of Aeronautics and Astronautics, Purdue Univ., West Lafayette, IN, Dec. 2010.
5. Disturbance Level Characterization of a Hypersonic Blowdown Facility
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