View Single Post
Old 07-13-2007, 22:26 PM   #41 (permalink)
gf0012-aust
Defense Professional
 
Join Date: 05-30-06
Posts: 394
Country:
Quote:
Originally Posted by pdf27 View Post
Mix of truth and rubbish there. The reason for variable inlets is that an oblique shockwave is more efficient than a perpendicular shockwave in slowing down air flows (less kinetic energy is converted into heat). These shockwaves are generated by turning the flow slightly.
Isn't there an issue of the reynolds effect as well? (as it applies to an inlet shock ramp rather than boundary layer issue?
gf0012-aust is offline   Reply With Quote