Supersonic WT

Infrastructure
Description

Weight and pressure measurement of 2D airfoils and 3 D scale models (mock-ups of airplanes, their parts, half-wings, missiles and other bodies that are exposed to high velocity effects in operation). Non-steady pressure measurement on these mock-ups. Probe calibration (static pressure and total pressure probes, directional sensors, ice-accretion probes, etc.). Pressure characteristics of new probes being developed at various angles of attack. Flow visualization

Contact Information
Prague (Czech Republic)
EREA