The patent application relates generally to methods of airfoil pressure instrumentation, and more particularly to a nondestructive method of applying and removing external pressure instrumentation to helicopter rotor blades without significantly affecting the aerodynamics of the blade and without damaging or altering the blade structure.
Nondestructive Method for Instrumenting Helicopter Rotor Blades
1977
17 pages
Report
Keine Angabe
Englisch
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