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High Reynolds Number Aerostructural Dynamics (HIRENASD)
HIRENASD
Pressure sensors
Project abstract and funding
Windtunnel (ETW)
Geometry windtunnel model
Test conditions
Wing material
Wing clamping and excitation
Measuring implementation
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| Wing material
Wing material
Temperature dependence of youngs modulus:
E(T) = 1.813e11 * (1. - 0.0416/181.3*(T-293.)) N/m
2
T: static temperature in Kelvin
Material data
© 2004-2011 by LFM | last change: 31.12.2010