Boundary layer transition impacts hypersonic vehicle performance more profoundly than low speed vehicle performance. Accurate prediction is difficult due to the sensitivity of transition to initial conditions. Computational tools continue to improve, but their use is limited largely to specialists. Ground testing continues to be a valuable tool, but new facility development is slow. Emphasis on transition control methods will increase as our understanding of the physics of hypersonic transition improves.
Trends in hypersonic boundary layer stability and transition research
Space technology and applications international forum -1999 ; 1999 ; Albuquerque, New Mexico (USA)
AIP Conference Proceedings ; 458 , 1 ; 1181-1188
22.01.1999
8 pages
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
X-33 hypersonic boundary layer transition
AIAA | 1999
|X-33 Hypersonic Boundary-Layer Transition
AIAA | 2001
|