Title :
Testing unmanned aerial vehicle airfoils
Author :
Lee, Tim ; Birch, Dave ; Gerontakos, Peter
Author_Institution :
Dept. of Mech. Eng., McGill Univ., Montreal, Que., Canada
Abstract :
The output of the MHFS is the most sensitive and definitive indicator of the state of the boundary layer and the locations of the various critical aerodynamic flow points and, therefore, serves conveniently as a primary diagnostic tool for boundary-layer flow directed aerodynamic properties for both static and unsteady low-Re airfoils. Caution, however, must be executed to evaluate and minimize the effects of "long" cable length or capacitance deriving from the distant sensor location to the data acquisition system, as frequently encountered in transonic wind tunnel tests. This caution also applies to the lead resistance, maximum sensitivity, change in sensor resistance with temperature and the degradation of the sensor outputs.
Keywords :
aerodynamics; boundary layers; data acquisition; laminar flow; laminar to turbulent transitions; remotely operated vehicles; sensors; signal processing; transonic flow; wind tunnels; MHFS; UAV; aerodynamic flow points; aerodynamic properties; boundary layer; boundary-layer flow; cable length effects; capacitance effects; data acquisition system; diagnostic tool; lead resistance; low-Reynolds number airfoils; maximum sensitivity; multiple hot-film sensor; sensor location; sensor output degradation; sensor resistance; transonic wind tunnel tests; unmanned aerial vehicle; Aerodynamics; Automotive components; Capacitance; Capacitive sensors; Communication cables; Data acquisition; Sensor systems; Temperature sensors; Testing; Unmanned aerial vehicles;
Journal_Title :
Instrumentation & Measurement Magazine, IEEE
DOI :
10.1109/MIM.2004.1337911