Read Effects of distributed roughness height on aerodynamic characteristics and boundary-layer transition of a wing-body-tail configuration at a Mach number of 1.61 (NASA technical note)

Effects of distributed roughness height on aerodynamic characteristics and boundary-layer transition of a wing-body-tail configuration at a Mach number of 1.61 (NASA technical note)

ROY V HARRIS

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Effects of distributed roughness height on aerodynamic characteristics and boundary-layer transition of a wing-body-tail configuration at a Mach number of 1.61 (NASA technical note)

Effects of distributed roughness height on aerodynamic characteristics and boundary-layer transition of a wing-body-tail configuration at a Mach number of 1.61 (NASA technical note)

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