Supersonic wind tunnel
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A supersonic wind tunnel is a wind tunnel that produces supersonic speeds (1.2

Restrictions for supersonic tunnel operation


Minimum required pressure ratio

Optimistic estimate: Pressure ratio \leq the total pressure ratio over normal shock at M in test section: \frac \leq\left(\frac\right)_ Examples:


Temperature effects: condensation

Temperature in the test section: \frac=\left(1+\fracM_m^2\right)^ with T_t = 330 K: T_m = 70 K at M_m = 4 The velocity range is limited by reservoir temperature


Power requirements

The power required to run a supersonic wind tunnel is enormous, of the order of 50 MW per square meter of test section cross-sectional area. For this reason most wind tunnels operate intermittently using energy stored in high-pressure tanks. These wind tunnels are also called intermittent supersonic blowdown wind tunnels (of which a schematic preview is given below). Another way of achieving the huge power output is with the use of a vacuum storage tank. These tunnels are called indraft supersonic wind tunnels, and are seldom used because they are restricted to low Reynolds numbers. Some large countries have built major supersonic tunnels that run continuously; one is shown in the photo. Other problems operating a supersonic wind tunnel include: *starting and unstart of the test section (related to maintaining at least a minimum pressure ratio) *adequate supply of dry air *wall interference effects due to shock wave reflection and (sometimes) blockage *high-quality instruments capable of rapid measurements due to short run times in intermittent tunnels Tunnels such as a Ludwieg tube have short test times (usually less than one second), relatively high Reynolds number, and low power requirements.


Further reading

* {{cite book , author1=Pope, A. , author2=Goin, K. , title=High-speed Wind Tunnel Testing , publisher=Krieger , year=1978 , isbn=0-88275-727-X


See also

* Subsonic and transonic wind tunnel#Subsonic tunnel, Low speed wind tunnel * Subsonic and transonic wind tunnel#Transonic tunnel, High speed wind tunnel * Hypersonic wind tunnel * Ludwieg tube * Shock tube


External links


Supersonic wind tunnel test demonstration (Mach 2.5) with flat plate and wedge creating an oblique shock(Video)
Fluid dynamics Aerodynamics Wind tunnels