Publication Date:
2019-06-28
Description:
Computer data are provided for tests conducted on a linear cascade of airfoils oscillating in pitch to measure the unsteady pressure response on selected blades along the leading edge plane of the cascade, over the chord of the center blade, and on the sidewall in the plane of the leading edge.
Keywords:
AERODYNAMICS
Type:
NASA-CR-165457-VOL-2-PT-2
Format:
application/pdf