국내 최대 기계 및 로봇 연구정보

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타이틀	Receptivity of Hypersonic Boundary Layers to Distributed Roughness and Acoustic Disturbances
저자	Balakumar, P.
Keyword	BOUNDARY LAYER STABILITY;; CONTINUOUS SPECTRA;; HYPERSONIC BOUNDARY LAYER;; LEADING EDGES;; SIMULATION;; SLENDER CONES;; SOUND WAVES;; STABILITY;; SURFACE ROUGHNESS;; SYNCHRONISM;; VORTICES
URL	http://hdl.handle.net/2060/20130003312
보고서번호	AIAA Paper 2013-0082
발행년도	2013
출처	NTRS (NASA Technical Report Server)
ABSTRACT	Boundary-layer receptivity and stability of Mach 6 flows over smooth and rough seven-degree half-angle sharp-tipped cones are numerically investigated. The receptivity of the boundary layer to slow acoustic disturbances, fast acoustic disturbances, and vortical disturbances is considered. The effects of three-dimensional isolated roughness on the receptivity and stability are also simulated. The results for the smooth cone show that the instability waves are generated in the leading edge region and that the boundary layer is much more receptive to slow acoustic waves than to the fast acoustic waves. Vortical disturbances also generate unstable second modes, however the receptivity coefficients are smaller than that of the slow acoustic wave. Distributed roughness elements located near the nose region decreased the receptivity of the second mode generated by the slow acoustic wave by a small amount. Roughness elements distributed across the continuous spectrum increased the receptivity of the second mode generated by the slow and fast acoustic waves and the vorticity wave. The largest increase occurred for the vorticity wave. Roughness elements distributed across the synchronization point did not change the receptivity of the second modes generated by the acoustic waves. The receptivity of the second mode generated by the vorticity wave increased in this case, but the increase is lower than that occurred with the roughness elements located across the continuous spectrum. The simulations with an isolated roughness element showed that the second mode waves generated by the acoustic disturbances are not influenced by the small roughness element. Due to the interaction, a three-dimensional wave is generated. However, the amplitude is orders of magnitude smaller than the two-dimensional wave.