Jul 2, 2003 #1 greebling Electrical Apr 2, 2003 17 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?
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?
Jul 4, 2003 #2 Sparweb Aerospace May 21, 2003 5,172 I just peeked in Anderson, Introduction to Flight, page 129. 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 Upvote 0 Downvote
I just peeked in Anderson, Introduction to Flight, page 129. 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
