Publication Date:
2019-07-13
Description:
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.
Keywords:
Fluid Mechanics and Thermodynamics; Numerical Analysis
Type:
NF1676L-18995
,
AIAA Science and Technology Forum and Exposition; Jan 05, 2015 - Jan 09, 2015; Kissimmee, FL; United States
Format:
application/pdf