Supersonic Wind Tunnel
Order Code: HD172
Category: Fluid Mechanics Lab
pressure curves in supersonic nozzles (Laval nozzle) pressure curves and losses in tunnel flows with Mach >1 observe shock waves in drag bodies using Schlieren optics determining the Mach number from the angle of the shock waves compar...
SPECIFICATION
pressure curves in supersonic nozzles (Laval nozzle)
pressure curves and losses in tunnel flows with Mach >1
observe shock waves in drag bodies using Schlieren optics
determining the Mach number from the angle of the shock waves
comparison of theory and experiment
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