[AE - 29] - Experimental Aerodynamics

0356 Test Section Flow Calibration Of The Wind Tunnel Of The Aeronautical Institute Of Technology”
1310 The research wind tunnel of the Aeronautical Institute of Technology: Manufacturing aspects and Design Details
1371 The Effect Of Wing Tip Blowing On The The Effect Of Wing Tip Blowing On The Vortex Drag
1375 Wind Tunnel Wall Boundary Layer control for attenuation of the interference on 2-D high lift wing tests
1569 Experimental study of the stability of the boundary layer over a rotating disk, with viscosity variations in the boundary layer


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