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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 forebody, isentropic compression ramp, leading-edge incidence angle = 8.33°, total turning angle = 18.51°. 

Experiment description
A complaint intake ramp deforms under the compression load and the resulting flow effects are observed in the isolator.

SBLI?
Yes

Thermal effects?
No