澳门马会传真

Wind Tunnel Testing

Wind Tunnel Testing

High-quality Wind tunnel test data
High-Quality Data
Agile Teams - Internal Aerodynamics
Agile Teams
Subsonic to Hypersonic Vertically Integrated testing
Vertically Integrated
Wind Tunnel Testing

Independently Owned & Operated Wind Tunnels from Subsonic to Hypersonic

澳门马会传真’s portfolio of 14 wind tunnels and propulsion development test stands are the only independently owned and operated facilities in the United States. Our teams are known for adaptability, flexibility, and responsiveness to customer needs. Whether it's to refine a test program or modify test models, 澳门马会传真 supports all phases of customer product development for a successful wind tunnel test.

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8T Transonic Wind Tunnel

Continuous Flow Variable Density Wind Tunnel operated in Buffalo, NY with 8 ft x 8 ft test section and wind speeds up to Mach 1.3

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Aerotest Laboratory

Aerodynamic test services for aerospace vehicles and propulsion system development located in Plymouth, MN

澳门马会传真 Wind Tunnel Technical Specifications

Operation Mode Test Tunnel Name Speed Regine Mach Range Test Section Size / Operation Feature
Closed Loop Continuous Flow Transonic Wind Tunnel Transonic M=0 to 1.3 8' x 8' Perforated Wall
Open Loop Continuous Flow Channel 19 & 20 Subsonic M=0.1 to 0.5 12" x 12" / Inlet Particle Separation
Open Loop Blow Down Channel 9 Hypersonic M=5 to 10 15" Diameter
Open Loop Blow Down Channel 2 Transonic M=1.5 to 4 13.5" DIameter
Open Loop Blow Down Channel 10 Transonic M=0.1 to 1.05 5.5' x 5.5' Slotted Wall
Open Loop Blow Down Channel 5 Static M=0.1 to 1.15 22" x 22" Slotted Wall
Open Loop Blow Down Channel 6 Static M=0 Cold Flow
Open Loop Blow Down Channel 7 & 8 Static M=0 Altitude
Open Loop Blow Down Channel 12 Static M=0 Cold Flow
Open Loop Blow Down Channel 11 & 14 Static M=0 Hot/Cold FLow
Open Loop Blow Down Channel 17 Static M=0 High Pressure Air Studies
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