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- W1569682632 abstract "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." @default.
- W1569682632 created "2016-06-24" @default.
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- W1569682632 date "1979-08-01" @default.
- W1569682632 modified "2023-09-22" @default.
- W1569682632 title "AGARD two-dimensional aeroelastic configurations" @default.
- W1569682632 hasPublicationYear "1979" @default.
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