论文信息 - Measurements in a transitional/turbulent Mach 10 boundary layer at high-Reynolds numbers. - 字舞流文

Measurements in a transitional/turbulent Mach 10 boundary layer at high-Reynolds numbers.

R. Watson | J. Anders | J. E. Harris

[1] J. Lagraff. Observations of Hypersonic Boundary-Layer Transition Using Hot Wire Anemometry , 1972 .

[2] F. Owen,et al. Experimental study of nozzle wall boundary layers at Mach numbers 20 to 47 , 1972 .