Accession Number : AD0430701


Title :   FORCE AND PRESSURE TESTS OF AN AGARD CALIBRATION MODEL B AT A MACH NUMBER OF 10,


Corporate Author : ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AIR FORCE STATION TENN


Personal Author(s) : Matthews,R K ; Trimmer,L L


Report Date : Feb 1964


Pagination or Media Count : 36


Abstract : The AGARD Calibration Model B, with and without wings, was tested at a nominal Mach number of 10. Force and moment coefficients were obtained over a range of pitch and yaw angles from -5 to 15.5 degrees with a Reynolds number range from 1.10 x 10 to the 6th power to 9.80 x 10 to the 6th power, based on model length. The lift-curve slope, aerodynamic center, and drag coefficients show excellent correlation with data from other tunnels at various Mach numbers. (Author)


Descriptors :   *WIND TUNNEL MODELS , STANDARDIZATION , CYLINDRICAL BODIES , PITCH(MOTION) , LIFT , DRAG , HYPERSONIC CHARACTERISTICS , ANGLES , CALIBRATION , PRESSURE


Distribution Statement : APPROVED FOR PUBLIC RELEASE