Three-dimensional wave packet in a Mach 6 boundary layer on a flared cone

C Hader, HF Fasel - Journal of Fluid Mechanics, 2020 - cambridge.org
High-resolution direct numerical simulations (DNS) were carried out to investigate the
nonlinear breakdown process of a three-dimensional wave packet initiated by a short …

Direct numerical simulations of the nonlinear boundary layer transition regime on a flat plate at Mach 6

M Leinemann, C Hader, HF Fasel - AIAA Scitech 2021 forum, 2021 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2021-1739. vid Direct Numerical
Simulations (DNS) were carried out in order to investigate the laminar-turbulent transition …

Numerical simulation of laminar-turbulent transition in a supersonic boundary layer under the action of acoustic disturbances

IV Egorov, AV Fedorov, NV Palchekovskaya - International Journal of Heat …, 2024 - Elsevier
In low disturbance environment, laminar-turbulent transition (LTT) is associated with
excitation of unstable normal modes of small initial amplitudes (receptivity problem). These …

Boundary layer transition on a generic model of control flaps in hypersonic flow

M Leinemann, R Radespiel, F Muñoz… - AIAA Scitech 2019 …, 2019 - arc.aiaa.org
I. Nomenclature αi= amplification rates [m-1] P= Pressure [Pa] f= frequency [kHz] Re=
Reynolds number PSD= Power Spectral Density [Pa2/Hz] L= Length of hollow cylinder [m] …

Wave packets on a flared cone at Mach 6

C Hader, HF Fasel - AIAA Scitech 2020 Forum, 2020 - arc.aiaa.org
Highly-resolved Direct Numerical Simulations (DNS) were carried out to investigate the
dominant nonlinear mechanisms of three-dimensional wave packets in a hypersonic …

Numerical study of total temperature effect on hypersonic boundary layer transition

J Zhao, S Liu, L Zhao, Z Zhang - Physics of Fluids, 2019 - pubs.aip.org
The total temperature in the hypersonic wind tunnel test can be significantly different from
that in real flight conditions, and this leads to a large discrepancy in the measurement of the …

Influence of nose-tip bluntness on conical boundary-layer instabilities at Mach 10

G Grossir, F Pinna, O Chazot - AIAA Journal, 2019 - arc.aiaa.org
Hypersonic boundary-layer transition experiments are performed at the von Karman Institute
for Fluid Dynamics in the low-enthalpy Longshot wind tunnel. Freestream Mach numbers are …

Direct numerical simulations of the nonlinear transition regime on a flat plate at Mach 6

M Leinemann, C Hader, HF Fasel - AIAA Scitech 2020 Forum, 2020 - arc.aiaa.org
F high-speed flows the boundary layer in the near wall region of a flow field has a vital
influence on heat loads, skin-friction drag and flow separation of an aerodynamic body. The …

[图书][B] Receptivity of Straight Blunt Cones to Broadband Freestream Pulse Disturbances for Transition Prediction in Hypersonic Flow

S He - 2022 - search.proquest.com
Traditional stability analysis for hypersonic flows has focused on the development and
relative amplification of a dominant disturbance mode, namely Mack's second mode …

Numerical Investigations of Boundary Layer Instabilities on a Blunt Swept Flat Plate at Mach 6

M Leinemann, AP Haas, C Hader… - AIAA AVIATION 2023 …, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-3557. vid Numerical Computations
are carried out in order to investigate the linear instability mechanisms for a hypersonic …