Joint Numerical and Experimental Investigation of Roughness Effect on Hypersonic 2nd Mode Instability and Transition

Abstract

This paper details a joint numerical and experimental investigation of transition-delaying roughness. A numerical simulation was undertaken to design a surface roughness configuration that would suppress Mack's 2nd mode instability in order to maintain laminar flow over a Mach 8 hypersonic blunt cone. Following the design process the roughness configuration was implemented on a hypersonic cone test article. Multiple experimental runs at the Mach 8 condition with different Reynolds numbers were run, as well as an off-design Mach 5 condition. The roughness did appear to delay transition in the Mach 8 case as intended, but did not appear to delay transition in the Mach 5 case. Concurrently, simulations of the roughness configuration were also computed for both Mach cases utilizing the experimental conditions. Linear stability theory was applied to the simulations in order to determine their boundary layer stability characteristics. This investigation of multiple cases helps to validate the numerical code with real experimental results as well as provide physical evidence for the transition-delaying roughness phenomenon.