D
EPARTMENT OF
A
EROSPACE AND
O
CEAN
E
NGINEERING
High-Speed Flow Research
Dr. Joseph A. Schetz
R
ESEARCH
Cascade Simulation of Multiple Shock Passing from Upstream Blade Rows in
Loss Mechanisms and Unsteady Flows in Turbomachines
Vortex Fuel Interaction for Enhanced Mixing in Supersonic Flow, AIAA 96-2661
F
ACILITIES
Hypersonic Wind Tunnel
Supersonic Wind Tunnel
Cascade Tunnel
Back to
AOE
Send comments and suggestions to
webmaster@aoe.vt.edu
Copyright © 1996 AOE Dept.,
Virginia Tech
All rights reserved world wide
