Hypersonic Boundary Layer Physics
Boundary layer formed on external vehicle surfaces:
Determines critical element of thermal load
Strongly affected by laminar/turbulent transition
Few reliable experiments (tunnel noise)
Affects flow entering the scramjet
Shock-boundary layer interactions
Critical element of engine unstart phenomenon
© Stanford University. All Rights Reserved. Stanford, CA 94305. (650) 723-2300. Terms of Use | Copyright Complaints