The aeroelastician needs reliable efficient methods for the calculation of unsteady aerodynamic forces in the frequency critical transonic speed regime. The development of such methods can be enhanced by the availability of a limited number of test cases for the comparison of competing methods. This report contains such test cases. Geometric descriptions of seven, two-dimensional airfoils and suggested aerodynamic conditions for each are included. (Author)
AGARD Two-Dimensional Aeroelastic Configurations
1979
18 pages
Report
No indication
English
Agard Three-Dimensional Aeroelastic Configurations
NTIS | 1982
|AGARD three-dimensional aeroelastic configurations
NTRS | 1982
|AGARD two-dimensional aeroelastic configurations
NTRS | 1979
|AGARD two-dimensional aeroelastic configurations
TIBKAT | 1979
|AGARD three-dimensional aeroelastic configurations
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