Wind-Tunnel Tests of Two-Dimensional Cable Fairings
DAVID TAYLOR MODEL BASIN WASHINGTON DC AERODYNAMICS LAB
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Nine two-dimensional cable fairings of various thicknesses and fineness ratios were tested at various Reynolds numbers in the 18 Supersonic Wind Tunnel. Pitching-moment coefficients were obtained for an angle-of-attack range of approximately -6 to 12 degrees for each model.
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