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Numerical Study of the High-Speed Leg of a Wind TunnelThe paper describes the numerical study of the high-speed leg of the NASA Langley 14 by 22-foot Low Speed Wind Tunnel. The high-speed leg consists of the Settling Chamber, Contraction, Test Section, and First Diffuser. Results are shown comparing two different exit boundary conditions and two different methods of determining the surface geometry.
Document ID
20160005931
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Nayani, Sudheer (Analytical Services and Materials, Inc. Hampton, VA, United States)
Sellers, William L., III (Analytical Services and Materials, Inc. Hampton, VA, United States)
Brynildsen, Scott E. (Vigyan Research Associates, Inc. Hampton, VA, United States)
Everhart, Joel L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
May 6, 2016
Publication Date
January 5, 2015
Subject Category
Fluid Mechanics And Thermodynamics
Numerical Analysis
Report/Patent Number
NF1676L-18995
Meeting Information
Meeting: AIAA Science and Technology Forum and Exposition
Location: Kissimmee, FL
Country: United States
Start Date: January 5, 2015
End Date: January 9, 2015
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 478076.07.27
Distribution Limits
Public
Copyright
Public Use Permitted.

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