Hypersonic impulse facilities
Impulse Test Facilities Shock Tube Diaphragm-less Shock Tube Combustion Driven Shock Tube
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Impulse Test Facilities Shock Tube Diaphragm-less Shock Tube Combustion Driven Shock Tube
Hypersonic Test Facilities: Continuous Hypersonic Wind Tunnel Heaters Hypersonic Nozzles Hypersonic Diffuser
A wind tunnel is a machine used to fly aircraft’s, missiles, engines, and rockets on the ground under pre-set conditions.…
DESCRIPTION Employing a unique nozzle design, all AEROLAB supersonic wind tunnels offer “on-the-fly” Mach number adjustability. Virtually all Aerospace and…
DESCRIPTION Using compressed air, AEROLAB Transonic Wind Tunnels offer running speeds of M=0.3 to M=1.3. Employing variable test section porosity,…
Wind tunnels are designed for a specific purpose and speed range. Therefore, there are many different types of wind tunnels and several different ways…
Lockheed Martin Missiles and Fire Control’s High Speed Wind Tunnel (HSWT) is a testing facility that characterizes the behaviors of…
Calibration Process Professional calibration of a probe is essential to achieve reliable measurement results. A calibration defines the relationship between…
pressure distribution This is used for studying pressure distribution across various models such as Airfoil, cylinder, special purpose shapes .…
A large number of physical parameters determine aerodynamic forces and moments. Specifically, the following parameters are involved in the production…
A wind tunnel is a tool used in aerodynamic research to study the effects of air moving past solid objects. A wind tunnel consists…