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Unique, clean-air, continuous-flow, high-stagnation-temperature facility for supersonic combustion researchAccurate, spatially-resolved measurements can be conducted of a model supersonic combustor in a clean air/continuous flow supersonic combustion facility whose long run times will allow not only the point-by-point mapping of flow field variables with laser diagnostics but facilitate the simulation of steady-state combustor conditions. The facility will provide a Mach 2 freestream with static pressures in the 1 to 1/6 atm range, and stagnation temperatures of up to 2000 K.
Document ID
19880065908
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Krauss, R. H. (Virginia Univ. Charlottesville, VA, United States)
Mcdaniel, J. C., Jr. (Virginia Univ. Charlottesville, VA, United States)
Scott, J. E., Jr. (Virginia Univ. Charlottesville, VA, United States)
Whitehurst, R. B., III (Virginia Univ. Charlottesville, VA, United States)
Segal, C. (Virginia, University Charlottesville, United States)
Date Acquired
August 13, 2013
Publication Date
July 1, 1988
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
AIAA PAPER 88-3059A
Accession Number
88A53135
Distribution Limits
Public
Copyright
Other

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