How to Calculate Nusselt Number for Hypersonic Vehicle?
Nusselt Number for Hypersonic Vehicle calculator uses Nusselt Number = (Local Heat Transfer Rate*Distance from Nose Tip to Required Base Diameter)/(Thermal Conductivity*(Adiabatic Wall Temperature-Wall Temperature)) to calculate the Nusselt Number, Nusselt Number for Hypersonic Vehicle is defined as the ratio of product of local heat-transfer rat and distance along the wall measured from the leading edge to the product of thermal conductivity at the edge of the boundary layer and difference of adiabatic wall temperature and wall temperature. Nusselt Number is denoted by Nu symbol.
How to calculate Nusselt Number for Hypersonic Vehicle using this online calculator? To use this online calculator for Nusselt Number for Hypersonic Vehicle, enter Local Heat Transfer Rate (qw), Distance from Nose Tip to Required Base Diameter (xd), Thermal Conductivity (k), Adiabatic Wall Temperature (Twall) & Wall Temperature (Tw) and hit the calculate button. Here is how the Nusselt Number for Hypersonic Vehicle calculation can be explained with given input values -> 1047.273 = (12000*1.2)/(0.125*(125-15)).