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Yes, there are many wind tunnels that offer testing rental services to designers like yourself. Costs vary depending on what speeds you are looking for and whether or not you provide the model. I recommend the wind tunnel laboratory at The Ohio State University. For daily and weekly rates, c...
The present work explores the use of NS-DBD plasma actuators for dynamic stall flow control over a NACA 0012 airfoil using an upgraded experimental setup in the Gas Dynamics and Turbulence Laboratory at Ohio State University's Aerospace Research Center. The reduced frequency (k) and excitation ...
LIFT, DRAG AND MOMENT OF A NACA 0015 AIRFOILby Steven D. MillerDEPARTMENT OF AEROSPACE ENGINEERINGTHE OHIO STATE UNIVERSITYi28 MAY 2008
windtunnellocatedatTheOhioStateUniversitymaincampus.Thisisalow turbulence,closed-loopatmosphericwindtunnelcapableoftunnelvelocitiesof40 m/s 1 andisdescibedindetailinreference2.ANACA0015airfoil,madeof compositematerialsandmountedinthecenterofthetestsectionwasusedforthis experiment.Theairfoilhasa8inchord,extendedthe...
LIFT, DRAG AND MOMENT OF A NACA 0015 AIRFOIL by Steven D. Miller DEPARTMENT OF AEROSPACE ENGINEERING THE OHIO STATE UNIVERSITY 28 MAY 2 8 i ABSTRACT A NACA 15 symmetrical airfoil with a 15% thickness to chord ratio was analyzed to determine the lift, drag and moment coefficients. A 2D ai...
D.,Dayton, Ohio.GEORGE W. LEWIS, Director of Aeronautical Rese 8、archJOHN f. VICTORY, SecretaryHENRY J. E. REID, Engineer-in-Charge, Langley Memorial Aeronautical Laboratory, Langley Field, Va.JOHN J. IDE, Technical Assistant in Europe, Paris, FranceTECHNICAL COMMITTEESAERODYNAMICS AIRCRAFT ...
Master’s Thesis, Mechanical Engineering, The Ohio State University, Columbus, OH, USA, 2011; pp. 25–30. [Google Scholar] Ahmed, T.; Amin, M.T.; Islam, S.M.R.; Ahmed, S. Computational study of flow around a NACA 0012 wing flapped at different flap angles with varying mach ...
Master’s Thesis, Mechanical Engineering, The Ohio State University, Columbus, OH, USA, 2011; pp. 25–30. [Google Scholar] Ahmed, T.; Amin, M.T.; Islam, S.M.R.; Ahmed, S. Computational study of flow around a NACA 0012 wing flapped at different flap angles with varying mach ...
1. First wing to run 330 mph in a 1/4 mile 2. First wing to run consistantly over 325 mph, 9 times 3. Quickest elapsed time (E.T.) for a quarter mile in Top Fuel history-4.48 seconds. Let me know how much it will cost for the update.Worth any amount it will cost." ...