Separation and transition on a cone-cylinder-flare: computational investigations

C Caillaud, S Esquieu, A Scholten, P Paredes… - AIAA SCITECH 2024 …, 2024 - arc.aiaa.org
Base flow computation and stability analysis were conducted for hypersonic flow over a
cone-cylinder-flare (CCF) geometry for conditions that correspond to the experimental runs …

Patterned Heating and Cooling for Second-Mode Control: Numerical–Experimental Comparison

S Kafle, T Kinnard, TJ Juliano, J Kuehl - AIAA AVIATION FORUM AND …, 2024 - arc.aiaa.org
The effects of experimentally feasible, patterned wall heating and cooling on the growth of
the second-mode instability are considered both numerically and experimentally. The study …

Multi-mode Instabilities Arising in Hypersonic Flow Conditions For Aerospace Applications

T Liang - 2024 - udspace.udel.edu
Research in hypersonic aerodynamics is important in understanding the practicality of
sustained high-speed flight and the design parameters of such vehicles. Hypersonic …

다공표면효과를반영한극초음속경계층선형안정성해석기법구축

박종형, 박동훈 - 한국항공우주학회지, 2024 - dbpia.co.kr
비행체 표면에서의 마찰항력과 열전달은 경계층의 상태와 매우 밀접하게 연관되기 때문에
극초음속 비행체의 열공력성능, 임무성능을 향상시키기 위한 경계층 천이 제어 연구가 큰 …