Working Group #1: Source of Scatter

Leads: Marshall Galbraith and Kevin Holst

This is similar to the traditional DPW approach for transonic flow on a static geometry. This group will concentrate on identifying the reasons for data scatter that was observed in DPW-VII.

Meeting Information

Meetings are held the second and fourth Tuesday of every month at 10:00 Eastern time.

Test Cases

Test Case 1a
ONERA OAT15A transonic airfoil
1a (Required): RANS analysis
Link to experimental data
Detailed Information

Test Case 1b
Joukowski subsonic airfoil
Detailed Information

Test Case 1c
ONERA OAT15A transonic airfoil
Detailed Information

Test Case 1d and 1e
DPW-III W1/W2 Wing Only
Detailed Information
Geometry

Test Case 2a
NASA CRM Wing/Body cruise configuration
Revision History:
- v2: updated typo in Cref (278.5in -> 275.8in)
- v3: updated typo in Tstatic (120degF -> 100degF)
Detailed Information (v3)

Test Case 2b
NASA CRM Wing/Body polar
Revision History:
- v2: Recommend addition of QCR2000
Detailed Information (v2)

Additional Test Cases

More information coming

NASA Official Responsible for Content
Brent W. Pomeroy

Last Updated
September 9, 2025