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High Reynolds Number Aerostructural Dynamics (HIRENASD)
HIRENASD
Pressure sensors
Project abstract and funding
Windtunnel (ETW)
Geometry windtunnel model
Test conditions
Test envelopes
Dynamical test conditions
Test protocol
Wing material
Wing clamping and excitation
Measuring implementation
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Test conditions
| Test envelopes
Test envelopes
Envelope Mach 0,80 (2008-04-21)
Envelope Mach 0,85 (2008-04-21)
Envelope Mach 0,88 (2008-04-21)
© 2004-2011 by LFM | last change: 31.12.2010
