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
-