Impinging SBLI Over Elastic Panel
06-NCSU/Duke U
Core details:
Institution
North Carolina State University
Duke University
Regime
Supersonic
Compliant model
Panel
Physics investigated
SWBLI
FSI or FTSI
FSI
General details:
Model configuration
Impinging SBLI, multiple shock generator angles, separated and unseparated SBLI, panel and rigid plate comparison Mach 2.5, two cavity pressure settings beneath the panel (1 atm and freestream pressure).Â
Experiment description
Roving hammer test characterization of the panel modes with measured pre-stress (used in wind tunnel experiment) and without pre-stress, Mean surface streakline patterns, mean panel surface pressure, 8 kHz panel surface pressure imaging, simultaneous velocity (2D,2C), panel surface pressure and center-span deflection at 10 Hz over SBLI.
SBLI?
Yes
Thermal effects?
No