Numerical study on drag reduction over highly blunted cones with aerodisk

In this paper effectiveness of aerodisk assemblies as retractable drag-reduction devices for large-angle blunt cones flying at hypersonic mach numbers is simulated numerically with a 120-deg apex-angle blunt cone at various angles of attack.

کلیدواژه ها:

drag reduction ، aerodisk ، numerical analysis ، hypersonic flow