aerodynamic heating
aerodynamic heating
(OP)
Is there a simple formula which will calculate the temperature at the tip of a radome, due to aerodynamic heating, when travelling at supersonic speeds?
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RE: aerodynamic heating
T1 = T0(1+1/2(gamma-1)M12)-1
To get an idea of what can happen, look up
http://www.hq.nasa.gov/office/pao/History/x15lect/structur.html
STF