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.
Experimental Data Base for Computers Program Assessment. Addendum. Report of the Fluid Dynamics Panel Working Group 04
1984
154 pages
Report
No indication
English
Aerodynamics , Aerodynamic configurations , Aerodynamic characteristics , Data bases , Experimental data , Swept wings , Supercritical wings , Aspect ratio , Far field , Pressure distribution , Transonic characteristics , Flight testing , Wind tunnel models , Two dimensional flow , Three dimensional flow , Supersonic flow , Mathematical models , Wing body configurations , Great Britain , Sweden , United States , Foreign technology , NATO furnished
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