02.2 - Experimental Aerodynamics
A STUDY OF WALL-INTERFERENCE EFECTS IN WIND-TUNNEL TESTING OF A STANDARD MODEL AT TRANSONIC SPEEDS
D. Damljanovic¹, D. Vukovic¹, G. Ocokoljic¹, J. Isakovic, College of Applied Engineering Studies, Serbia; B. Rasuo, University of Belgrade, Serbia; ¹Military Technical Institute (VTI), Serbia
On the basis of results of tests with a standard model in the T-38 wind-tunnel correlated with AEDC interference-free data it was concluded that, for a typical model of about 0.5%-0.6% blockage at a moderate range of angles of attack, T-38 transonic data can be considered to be practically interference-free.