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11-Foot Transonic Unitary Plan Facility
11-Foot Transonic Unitary Plan Facility Home
Quick Facts
Characteristics
Acquisition
Contact Information
Gallery
Facility Fact

Two weeks of model build up and instrument preparation are included in the facility occupancy charge.



Fighter model mounted in the 11-Foot Transonic Unitary Plan Facility at ARC Boeing 777 model in 11ft w.t.; test-168; with wind tunnel technician Danny Ompoc
Facility Characteristics
11x11 TWT Characteristics
Speed:
Mach 0.20 to 1.45
Reynolds Number:
0.30 - 9.6 x 106 per foot
Pressure:
3.0 to 32.0 lbs. per square inch
Temperature:
100 ± 20°F
Test Gas:
Ambient atmosphere
Test Section Size:
11 feet high by 11feet wide
Length:
22 feet
Area:
121 square feet
 
Further Information
NASA's ATP Program
Read about one of the largest, most versatile and comprehensive set of testing facilities in the nation.
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11-Foot Transonic Unitary Plan Facility
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NASA Ames Windtunnels
Get further information about the 9'x7' SWT and 11'x11' TWT facilities at NASA Ames.
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"The right facility at the right time" - NASA Aeronautics Test Program




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NASA Official: Tony Springer
Last Updated: October 17, 2011
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