A review of measurements on AGARD calibration models
North Atlantic Treaty Organization, Advisory Group for Aeronautical Research and Development, 1961 - Mathematics - 245 pages
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AEDC AGARD Calibration Model AGARD Model agreement angle of attack Arnold Engineering Development base drag coefficient base pressure blockage ratio body diameters Body of Revolution boundary layer transition carborundum coefficient versus Mach Comparison of data data with reference different Reynolds numbers different sting downwash drag coefficient versus Engineering Development Center estimated fins fixed transition flight flow forebody drag coefficient free stream half-model heat transfer horizontal tail influence laminar leading edge lift coefficient lift-curve slope Mach number range mean aerodynamic chord model nose NACA NACA TN natural transition North American Aviation parameters pitching pressure distribution pressure drag reference curve results of test Reynolds number based shock wave shown in Figure skin friction sting configuration sting diameter sting length Table test section total drag transition fixed transition point transonic drag rise Transonic Wind Tunnel tunnel wall turbulent boundary layer values Variation various tests versus Mach number VOVN