| タイトル | AGARD two-dimensional aeroelastic configurations |
| 著者（英） | Bland, S. R. |
| 著者所属（英） | Advisory Group for Aerospace Research and Development; NASA Langley Research Center |
| 発行日 | 1979-08-01 |
| 言語 | eng |
| 内容記述 | 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. |
| NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 80N10202
AGARD-AR-156
AD-A075104 |
| 権利 | Copyright, Distribution within the U.S. granted by agreement |
|
