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)
semi-annual report for the period March 16, 1983 to September 14, 1983
By H. T. Nagamatsu
Publish Date
1983
Publisher
NASA Langley Research Center
Language
eng
Pages
-
1-2 of 2 Editions
Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction
Language: eng
Published In: 1983
Publisher: NASA Langley Research Center
Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction
Language: eng
Published In: 1983
Publisher: NASA Langley Research Center