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
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
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![ImgDesc](/var/file/77/1077/pictures/209/m/mcen700x700_large70595_735663703413.jpg)
![ImgDesc](/var/file/77/1077/pictures/209/m/mcen700x700_large70596_915620703413.jpg)