Full Pseudospectral Solution to the Euler Equations of Motion for Airfoil Flow at Transonic Speeds.
NAVAL RESEARCH LAB WASHINGTON DC
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The unsteady Euler equations of motion are solved for by full psuedospectral computational techniques. flows about a five percent half thick biconvex airfoil are obtained. Subcritical and supercritical cases are treated. Keywords Chebyshev Pseudospectral solutions Two dimensional Airfoils.
- Fluid Mechanics