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Performance Data: 31″ Mach 10 Air Facility
Test Gas: Dry Air
Stag. Pres. (psi): 150 to 1450
Stag. Temp. (R): 1850
Mach Number: 10
Reynolds Number (/ft): 0.2 to 2.2 x 106
Dynamic Pressure (psi): 0.65 to 2.4
Shock Density Ratio: 6.0
Test Core Size (in): 14 by 14
Max Run Time (sec): 120
Performance Data: 20″ Mach 6 Air Facility
Test Gas: Dry Air
Stag. Pres. (psi): 30 to 475
Stag. Temp. (R): 760 to 940
Mach Number: 6
Reynolds Number (/ft): 0.5 to 8.0 x 106
Dynamic Pressure (psi): 0.51 to 7.6
Shock Density Ratio: 5.3
Test Core Size (in): 14 by 14
Max Run Time (sec): 900
Performance Data: 15″ Mach 6 Air Facility
Test Gas: Dry Air
Stag. Pres. (psi): 50 to 450
Stag. Temp. (R): 940 to 1260
Mach Number: 6
Reynolds Number (/ft): 0.5 to 6.0 x 106
Dynamic Pressure (psi): 0.8 to 6.8
Shock Density Ratio: 5.3
Test Core Size (in): 10 (dia)
Max Run Time (sec): 120
Langley Aerothermodynamics Laboratory Fact Sheet
