The aeroelastician needs reliable and efficient methods for the calculation of unsteady aerodynamic forces in the frequently critical transonic speed regime. The development of such methods may be enhanced by the availability of a limited number of test cases for the comparison of competing methods. This report contains such test cases for five clean, isolated wings. Wing geometric descriptions, airfoil coordinates, and suggested aerodynamic conditions for each are included. (Author)
AGARD Three-Dimensional Aeroelastic Configurations
1982
19 pages
Report
No indication
English
AGARD three-dimensional aeroelastic configurations
NTRS | 1982
|Agard Three-Dimensional Aeroelastic Configurations
NTIS | 1982
|AGARD three-dimensional aeroelastic configurations
TIBKAT | 1982
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