The development of reliable, efficient methods for the calculation of unsteady aerodynamic forces in the frequency-critical transonic speed regime can be enhanced by the availability of a limited number of test cases for the comparison of competing methods. Seven test cases are presented for airfoils with thickness from 6.0% to 16.5%: a biconvex parabolic arc airfoil, three conventional airfoils, and three cambered supercritical airfoils. The aerodynamic conditions such as Mach number, mean angle of attack, and oscillation amplitude and frequency are also given. Recommendations are made for uniformity in definition and reporting to enhance desired comparison for the aeroelastician.
AGARD two-dimensional aeroelastic configurations
1979-08-01
Preprint
No indication
English
AGARD three-dimensional aeroelastic configurations
NTRS | 1982
|Agard Three-Dimensional Aeroelastic Configurations
NTIS | 1982
|AGARD two-dimensional aeroelastic configurations
TIBKAT | 1979
|AGARD Two-Dimensional Aeroelastic Configurations
NTIS | 1979
|AGARD three-dimensional aeroelastic configurations
TIBKAT | 1982
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