The 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.
Numerical Study of the High-Speed Leg of a Wind Tunnel
AIAA Science and Technology Forum and Exposition ; 2015 ; Kissimmee, FL, United States
2015-01-05
Conference paper
No indication
English
Numerical Study of the High-Speed Leg of a Wind Tunnel
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