论文信息 - Flow characteristics of the NASA-Ames laminar supersonic wind tunnel for Mach 1.6 operation - 字舞流文

Flow characteristics of the NASA-Ames laminar supersonic wind tunnel for Mach 1.6 operation

Stephen W. D. Wolf | James A. Laub | Lyndell S. King

[1] I. E. Beckwith,et al. Supersonic and hypersonic quiet tunnel technology at NASA Langley , 1992 .

[2] Stephen W. D. Wolf,et al. An efficient supersonic wind tunnel drive system for Mach 2.5 flows , 1991 .

[3] I. E. Beckwith,et al. Mean flow and noise measurements in a Mach 3.5 pilot quiet tunnel , 1982 .

[4] A. Johansson,et al. Turbulence reduction by screens , 1988, Journal of Fluid Mechanics.

[5] H. L. Dryden,et al. The Use of Damping Screens for the Reduction of Wind-Tunnel Turbulence , 1947 .

[6] H. Nagib,et al. Interaction of free-stream turbulence with screens and grids: a balance between turbulence scales , 1982, Journal of Fluid Mechanics.

[7] Stephen W. D. Wolf,et al. Development of the NASA-Ames Low-Disturbance Supersonic Wind Tunnel for transition studies at Mach 1.6 , 1994 .

[8] Anthony Demetriades,et al. Comparison of predictions with measurements for a quiet supersonic tunnel , 1993 .

[9] J. Laufer,et al. Factors Affecting Transition Reynolds Numbers on Models in Supersonic Wind Tunnels , 1954 .