JSM EXPERIMENTAL DATA: Forces and Moment
AIAA CFD High Lift Prediction Workshop
Some relevant force and moment experimental wind tunnel data for the JSM (in landing
configuration, single segment baseline slat and single segment 30 deg flap) are given here.
Both body and wing are included in the experimental forces and moment. The
conditions are Re=1.93 million per mean aerodynamic chord, M=0.172.
NOTE: JAXA naming convention "Case 1" in the following refers to the JSM with Nacelle/Pylon OFF.
This corresponds to Workshop Test Cases 2a and 2b.
NOTE: JAXA naming convention "Case 2" in the following refers to the JSM with Nacelle/Pylon ON.
This corresponds to Workshop Test Cases 2c and 2d.
Experimental Data Files:
When running CFD in free-air conditions, the CORRECTED data
should be used for comparison.
The following data file gives DELTAS (Case 2 minus Case 1), derived from
the corrected data:
Return to: Experimental Data Top Page
Return to: High Lift Prediction Workshop Home Page
Recent significant updates:
04/13/2017 - Added "Case2-Case1_ForceMoment.dat" file and corresponding plot
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Last Updated: 04/13/2017