Nosetip bluntness effects on a cone-cylinder-flare at mach 6
A cone-cylinder-flare model with sharp and blunt nosetips was tested at the AFRL Mach-6
Ludwieg Tube at a 0\(^{\circ}\) angle of attack. Surface-pressure fluctuation measurements …
Ludwieg Tube at a 0\(^{\circ}\) angle of attack. Surface-pressure fluctuation measurements …
Transition to turbulence in hypersonic flow over a compression ramp due to upstream forcing
Several transition scenarios are present in a hypersonic compression-ramp flow. In our
previous work (Cao et al., J. Fluid Mech., vol. 941, 2022, p. A8), a complete transition …
previous work (Cao et al., J. Fluid Mech., vol. 941, 2022, p. A8), a complete transition …
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 …
cone-cylinder-flare (CCF) geometry for conditions that correspond to the experimental runs …
Understanding the instability-wave selectivity of hypersonic compression ramp laminar flow
The hypersonic flow stability over a two-dimensional compression corner is studied using
resolvent analysis, linear stability theory (LST) and parabolised stability equation (PSE) …
resolvent analysis, linear stability theory (LST) and parabolised stability equation (PSE) …
Focused Laser Differential Interferometry Performance Over an Axisymmetric Model
A direct numerical simulation (DNS) of a transitional hypersonic boundary layer about an
axisymmetric model was conducted and probed by a simulated focused laser differential …
axisymmetric model was conducted and probed by a simulated focused laser differential …