Experimental determination of the boundary layer at air-sample inlet positions on the NASA CV 990 aircraftFull-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.
Document ID
19840038495
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bowen, S. W. (San Jose State University San Jose, CA, United States)
Vedder, J. F. (San Jose State Univ. CA, United States)
Condon, E. P. (NASA Ames Research Center Moffett Field, CA, United States)