Publication Date:
2019-06-28
Description:
Full-scale, in-flight measurements of the boundary-layer thickness, velocity profile, and flow angle have been made at several sample collection stations on the fuselage of the NASA CV 990. These results are given as functions of Mach number, Reynolds number, yaw, and angle of attack.
Keywords:
AERODYNAMICS
Type:
AIAA PAPER 84-0028
Format:
text
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