Theoretical Errors on Airborne Measurements Of: Static Pressure, Impact Temperature,air Flow Angle, Air Flow Speed

Report on a complete theory development that gives an exact calculation for all angles with irrotational flow around a sphere, the easiest shape for a nose radome which includes a few examples of axisymmetric calculations wherein four kinds of errors are approached: - static pressure and pressure coefficient, - impact temperature and pressure coefficient, - airflow angles and angle of sideslip, and - airflow speed and total pressure on radome.