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Supersonic WT

RI-106
Wind Tunnel
Infrastructure
VZLU
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)
jelinek@vzlu.cz
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  • About
    • About EREA
    • Members
    • Organisation
    • EREA in Flightpath 2050
    • Events
    • Position Papers
    • Publications
    • Vacancies
    • Contact us
  • Capabilities
  • Technology Infrastructures
    • TRIG
    • Catalogue
  • European Cooperation
  • Future Sky
  • News
  • Intranet
EREA