Publication Date:
2019-06-28
Description:
Aerodynamic characteristics obtained in a helical flow environment utilizing a rotary balance located in the Langley spin tunnel are presented in plotted form. The configurations tested included the basic airplane, various control deflections, two canard locations, and wing leading edge modifications, as well as airplane components.
Keywords:
AERODYNAMICS
Type:
NASA-CR-3170
Format:
application/pdf