 Range equation is a fundamental equation in aircraft design that describes the distance an aircraft can travel with a given amount of fuel. The formula for the range (R) of an aircraft is: R is the range, V is the velocity of the aircraft, and D is the drag force acting on the aircraft The […]
The coefficient of pressure, often denoted as Cp, is a dimensionless quantity used in aerodynamics to describe the distribution of pressure over the surface of an object, such as an aircraft wing The formula for the coefficient of pressure (Cp) is given by: Cp​ is the coefficient of pressure. p is the local
Coefficient of Pressure Calculator Read More »
