Experimental Data Base for Computers Program Assessment. Addendum. Report of the Fluid Dynamics Panel Working Group 04.
Abstract
Contents: Transonic Wing and Far Field Test Data on a High Aspect Ratio Transport Wing for Three Dimensional Computational Method Evaluation; Transonic Wing and Far Field Test Data on a Moderate Aspect Ratio Wing for Three Dimensional Computational Method Evaluation; Pressure Distributions Measured on Research Wing M100 Mounted on an Axisymmetric Body; Pressure Distribution Measured on Research Wing M86 Mounted on an Axisymmetric Body; and Pressure Distribution on a Swept Wing Aircraft in Flight.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 01, 1984
- Accession Number
- ADA147197
Entities
Organizations
- AGARD