Shock on a Cantilevered Plate
02-2020
Core details:
Institution
UNSW Canberra
University of Southern Queensland
Regime
Hypersonic
Compliant model
Cantilever
Physics investigated
SWBLI
FSI or FTSI
FSI
General details:
Model configuration
Cantilevered, trailing-edge, compliant plate, AOA = 0°, 10° shock deflection angle.Â
Experiment description
A low aspect-ratio cantilevered panel oscillates upon shock impingement.
SBLI?
Yes
Thermal effects?
No