Abstract
The idea of experimental data assimilation is investigated in the context of aerodynamic computations of turbulent compressible flows over airfoils. Two cases are considered: the subsonic flow around the ONERA-A airfoil; and the transonic flow around the RAE-2822 airfoil. The wall pressure-coefficient distribution, and the velocity and turbulent kinetic energy profiles are observed at various positions over the airfoil.
Original language | English |
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Pages (from-to) | 611-614 |
Number of pages | 4 |
Journal | Journal of Aircraft |
Volume | 36 |
Issue number | 3 |
DOIs | |
Publication status | Published - 1 Jan 1999 |
Externally published | Yes |