- #1
physwil90
- 8
- 0
I am currently constructing a supersonic rocket and am trying to empirically calculate the heat transferred onto all different parts of the missile body to know what materials to buy. However, I do not know how to calculate the heat transferred onto the fins of the rocket as it travels (the fins will be cut at an angle let's say about 45). In order to properly find this I will need to know the heating rate at each point of flight in the rocket. Is there any equation for this concerning missile fins? Any help would be great...