NACA-RM-A51C14 : A semi-empirical method for calculating the pitching moment of bodies of revolution at low Mach numbers
سازمان: NASA - National Aeronautics and Space Administration (NASA)
کلید واژه: AERODYNAMIC , BODIES , FLOW , THEORY , VISCOUS
سال: 1951
زبان: English
قیمت: 55000 تومان
افزودن به سبد خرید
A semiempirical method, in which potential theory is arbitrarily combined with an approximate viscous theory, for calculating the aerodynamic pitching moments for bodies of revolution is presented. The method can also be used for calculating the lift and drag forces. The calculated and experimental force and moment characteristics of 15 bodies of revolution are compared.