Boeing Technology Services - Aerodynamics
Transonic Wind Tunnel
The Boeing Transonic Wind Tunnel delivers continuous flow from Mach 0.3 up to Mach 1.1.
- Test section: 8 ft by 12 ft with 2 ft corner fillets (14.5 ft long)
- Dynamic pressure range: 0 to 840 lb/ft2
- Stagnation temperature (TT) controllable 80°F to 130°F. Nominal is 100°F
- Dew point is controllable. +3°F or lower
- Reynolds Number varies with Mach. 4.386 million/ft at M=1.1 and TT=100°F
- Sting, swept strut, plate, and floor mountings
- Internal and external balances
- Electronic pressure scanning up to 1536 ports and an inventory of EPS modules of appropriate load capacity
- Qualitative and quantitative flow imaging tools
- An airflow calibration facility is available for calibration of ducts, flow-thru nacelles, and powered nacelles
If you would like to join the companies using the testing resources available at The Boeing Company, contact the Boeing Technology Services Marketing Manager Ms. LeAnn Diessner at 206-662-4287, request a quote online, or e-mail us for more information about our test capabilities.