Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction

An edition of Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction (1983)

Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction

semi-annual report for the period March 16, 1983 to September 14, 1983

By H. T. Nagamatsu

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Publish Date

1983

Publisher

NASA Langley Research Center

Language

eng

Pages

Description:

subjects: Boundary layer control, Aerofoils, Drag reduction, Supercritical wings, Shock waves