A Wind Tunnel Study of a Sting-Mounted Circulation Control Wing

This wind tunnel study investigated the feasibility of testing a sting mounted circulation control wing. A 20% thick, 8.5% cambered rectangular wing was designed, built, and tested in the AFIT 5-ft wind tunnel. Lift, drag, equivalent drag, and pitching moment coefficients were obtained at Reynolds n...

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Bibliographische Detailangaben
1. Verfasser:	Trainor, John W
Format:	Report
Sprache:	eng
Schlagworte:	Aerodynamics AIR FLOW AIR SUPPLIES BLOWERS CIRCULATION CONTROL WING COEFFICIENTS DISPLAY SYSTEMS DRAG FEASIBILITY STUDIES FLOW FLOW VISUALIZATION FREE STREAM IMPINGEMENT JET FLOW MOMENTS MOMENTUM NYLON PITCH(MOTION) THESES TRAILING EDGES V/STOL VERTICAL TAKEOFF AIRCRAFT WIND TUNNELS WINGS
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