NASA NTRS · 19820019356
AGARD three-dimensional aeroelastic configurations
Abstract
The calculation of unsteady aerodynamic forces in the critical transonic speed regime is investigated. The development of such methods is be enhanced by the availability of a limited number of test cases for the comparison of competing methods. Test cases for five clean, isolated wings are presented. Wing geometric descriptions, airfoil coordinates, and suggested aerodynamic conditions for each are included.
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Bland, S. R.. 1982-03-01. AGARD three-dimensional aeroelastic configurations. https://ntrs.nasa.gov/citations/19820019356
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