NASA technical note TN (series). D-2334. Effects of distributed roughness height on aerodynamic characteristics and boundary-layer transition of wing-body-tail configuration at Mach number of 1.61 [with list of references]; by Roy V. Harris, jr.
Publication Title:
Effects of distributed roughness height on aerodynamic characteristics and boundary-layer transition of wing-body-tail configuration at Mach number of 1.61 [with list of references]; by Roy V. Harris, jr.
Display Title:
NASA technical note TN (series). D-2334. Effects of distributed roughness height on aerodynamic characteristics and boundary-layer transition of wing-body-tail configuration at Mach number of 1.61 [with list of references]; by Roy V. Harris, jr.