#aerothermo #intro

$M<0.3$ air is approximately incompressible
neither supersonic or subsonic theories work in the transonic range

# topics
oblique shocks and expansion waves
nozzle flow
high speed aerodynamics??
heat transfer

20% coursework
80% in person
5 BB tests at 2% each, 3 attempts at each of them
10% nozzle design exercise
![[Pasted image 20231005170302.png]]
[[textbook.pdf]] 

# links
[shock calculator](https://devenport.aoe.vt.edu/aoe3114/calc.html)