Pressure gradient effects on wake-flow instabilities behind isolated roughness elements on re-entry capsules
Autor: | Alexander Theiss, Stefan Hein, Sascha Leyh |
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Rok vydání: | 2019 |
Předmět: |
linear stability theory
020301 aerospace & aeronautics Hypersonic speed Disturbance (geology) Materials science Linear stability theory Hochgeschwindigkeitskonfigurationen GO Mechanical Engineering Re entry Aerospace Engineering 02 engineering and technology Mechanics Surface finish blunt body Wake 01 natural sciences Laminar-to-turbulent transition re-entry capsule 010305 fluids & plasmas roughness-induced transition Physics::Fluid Dynamics 0203 mechanical engineering 0103 physical sciences LST-2D Pressure gradient |
Zdroj: | Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 234:28-41 |
ISSN: | 2041-3025 0954-4100 |
DOI: | 10.1177/0954410019844067 |
Popis: | Laminar-turbulent transition caused by modal disturbance growth in the wake flow of isolated roughness elements on blunt re-entry capsules is studied numerically at typical cold hypersonic wind-tunnel conditions. Two fundamentally different heat shield shapes are considered. On the sphere-cone forebody the wake flow of the roughness is exposed to an adverse pressure gradient, whereas the spherical heat shield exhibits a strongly favorable pressure gradient. The pressure gradient effects on the development of the stationary wake flow and its modal instability characteristics are discussed for various heights and diameters of the cylindrical roughness element. Regions of increased shear develop in its wake, which persist longer in the adverse pressure gradient case. Consequently, the results of spatial two-dimensional eigenvalue analyses reveal that the unstable wake-flow region extends much further downstream and the wake-mode instabilities are considerably more amplified. The disturbance kinetic energy production terms are used to assess the contributions of the different shear-layer regions to the mode growth and its dependence on the pressure gradient. |
Databáze: | OpenAIRE |
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