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Blockage Testing in the NASA Glenn 225 Square Centimeter Supersonic Wind TunnelThe starting characteristics for three different model geometries were tested in the Glenn Research Center 225 Square Centimeter Supersonic Wind Tunnel. The test models were tested at Mach 2, 2.5 and 3 in a square test section and at Mach 2.5 again in an asymmetric test section. The results gathered in this study will help size the test models and inform other design features for the eventual implementation of a magnetic suspension system.
Document ID
20170005183
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Sevier, Abigail (Case Western Reserve Univ. Cleveland, OH, United States)
Davis, David O. (NASA Glenn Research Center Cleveland, OH United States)
Schoenenberger, Mark (NASA Langley Research Center Hampton, VA United States)
Date Acquired
June 6, 2017
Publication Date
January 9, 2017
Subject Category
Aeronautics (General)
Report/Patent Number
GRC-E-DAA-TN38535
Report Number: GRC-E-DAA-TN38535
Meeting Information
Meeting: SciTech 2017
Location: Grapevine, TX
Country: United States
Start Date: January 9, 2017
End Date: January 13, 2017
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 470883.04.03.02.02
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
entry vehicles
blockage testing
wind tunnel

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