The ONERA OAT15A airfoil is being used for Test Case 1: Solver Validation. Use of
the ONERA OAT15A airfoil is subject to the following conditions
- The geometry remains the intellectual property of ONERA
- The geometry shall be referred to as the "ONERA OAT15A"
- ONERA will be acknowledged each time the geometry is shared with a partner
- When shared by a user, the above conditions will be included
The geometry, discrete coordinates, and an iges file, are available
for download. Participants are
strongly encouraged to use the provided iges file (ONERA-OAT15A_230mmChord_780mmSpan_upZ_2024_09_05.igs)
as great care has been taken to develop a carefully-crafted geometry with good
curvature behavior.
Common Research Model
A large portion of Common Research Model used for the DPW-8/AePW-4 geometry is the same
as was utilized in DPW-7. The link to these geometry files is as follows.
DPW-7 Geometry Website
National Transonic
Facility Test Section
The test section geometry for the NTF has been released.
NTF_highspeedleg_definition_v1p6.zip (October 16, 2024)
NASA Official Responsible for Content
Brent W. Pomeroy
Last Updated
September 6, 2024
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