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Langley Research CenterTurbulence Modeling Resource |
Exp: CFDVAL2004 Case 2 Geometry
Return to: CFDVAL2004 Case 2 - Intro Page
Return to: CFDVAL2004 - Intro Page Return to: Data from Experiments - Intro Page Return to: Turbulence Modeling Resource Home Page
The hole for the jet is located at the bottom of a wind tunnel test section
15.0 inches (381.00 mm) wide by approximately 9.81 inch (249.17 mm) high
(distance from the splitter plate to the top wall). The
height of the top wall is adjusted down the length of the test section to yield
a flow with an approximately zero streamwise pressure gradient.
The following links point to two CAD files for the Case 2 geometry,
one in IGES format, and one in UG (Unigraphics V.18) format (note that
the UG file is not a formatted file):
Note that the geometry information is based on theoretical (planned,
blueprint-type) specifications. If available, QA data will be given to
show differences between the theoretical and as-built configurations.
Return to: CFDVAL2004 Case 2 - Intro Page
IGES FILE (114 Kb)
UG FILE (82 Kb)
Responsible NASA Official:
Ethan Vogel
Page Curator:
Clark Pederson
Last Updated: 05/15/2021