Jump to the main content block

Transonic Flow Studies

▼ASTRC/NCKU Wind Tunnel
Blow down type
Test section: 600 mm x 600 mm
Mach number: 0.2-1.4
Test time: up to 30 seconds
Reynolds number: up to 4 x 107 per meter

▼Characteristics of Transonic Rectangular Cavity Flows
▼Shock Excursion and Boundary Layer Separation of Compressible Convex-corner Flows
▼Aerodynamic Characteristics of a Ogive Cylinder at High Angles of Attack with Lateral Jet Control
▼Development of Experimental Techniques