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1. Porous Bleed Boundary Conditions for Supersonic Flows With & Without Shock-Boundary Layer Interaction

   This paper aims to evaluate the prediction accuracy of various porous bleed models on two flow cases of particular interest for supersonic...

   Julian Giehler, Pierre Grenson, Reynald Bur in Flow, Turbulence and Combustion

   Article 07 August 2023
   

2. Swept shock/boundary-layer interaction control using micro-vortex generators

   Passive flow control devices, such as vortex generators (VGs), have shown to be successful in controlling flows associated with...

   A. Khan, M. Chidambaranathan, ... R. Kumar in Shock Waves

   Article 01 December 2023
   

3. Simulation of High-Enthalpy Turbulent Shock Wave/Boundary Layer Interaction Using a RANS Approach

   In the era of space exploration, the scientific community is strongly focusing on the analysis of hypersonic flows in the presence of shock...

   Davide Ninni, Francesco Bonelli, Giuseppe Pascazio in Aerotecnica Missili & Spazio

   Article Open access 30 August 2023
   

4. Flow structures and unsteadiness in hypersonic shock wave/turbulent boundary layer interaction subject to steady jet

   Direct numerical simulations of Mach 6 hypersonic flow over a 34° compression corner subject to steady jet are conducted. Distributions of skin...

   Qiang Liu, Wei **e, ... Yan Zhou in Acta Mechanica Sinica

   Article 08 October 2023
   

5. Flow Control Using MVG in Shock Wave/Boundary Layer Interaction

   This review study mainly focusses on micro vortex generator (MVG) as a flow control device for shock wave/boundary layer interaction. The flow...

   N. Nishantt, Nikhil A. Baraiya in Recent Advances in Fluid Dynamics

   Conference paper 2023
   

6. Effects of Flow Pulsation on Shock Wave/Boundary Layer Interaction in Supersonic Isolator

   In scramjet engine, inlet isolator is used to provide stable compressed flow to the combustors. A series of oblique shocks are used to compress the...

   Sardar Nafis Bin Ali, Abu Baker Siddque Rimon, A. B. M. Toufique Hasan in Solutions for Maintenance Repair and Overhaul

   Conference paper 2024
   

7. On the investigation of shock wave/boundary layer interaction with a high-order scheme based on lattice Boltzmann flux solver

   Shock wave/boundary layer interaction (SWBLI) continues to pose a significant challenge in the field of aerospace engineering. This paper aims to...

   Jian Qin, Haichuan Yu, Jie Wu in Advances in Aerodynamics

   Article Open access 26 February 2024
   

8. Study of unsteadiness due to 3-D shock–boundary layer interaction in flow over a square-faced protuberance

   The dynamics of shock-induced unsteady separated flow past a three-dimensional square-faced protuberance are investigated through wind tunnel...

   K. Ramachandra, S. Bhardwaj, ... R. Sriram in Shock Waves

   Article 01 December 2023
   

9. Relationship between secondary separation and surface pressure structure in swept shock-wave/boundary-layer interaction

   A theoretical analysis is presented to elucidate the relationship between the skin friction topology of the secondary separation bubble and surface...

   T. Liu, D. M. Salazar, ... A. Baldwin in Shock Waves

   Article 01 October 2022
   

10. Visualization study of perturbations induced by plasma actuators and its effect on shock wave/boundary-layer interaction

    Abstract

    Surface arc plasma actuator array is used to control the shock wave/boundary-layer interaction in a Ma = 2 flow. Two types of interaction are...

    Tian Gan, Qiong Wang, ... Zhang Jieming in Journal of Visualization

    Article Open access 27 November 2022
    

11. Matched asymptotic shock-layer analysis of the interaction between a planar viscous-hypersonic boundary layer and a thin inviscid layer

    Abstract

    A compressible boundary-layer flow over a flat plate with sharp leading edge is studied in the hypersonic limit. The interaction between the...

    Thomas Ward, Eli Shellabarger, Sampson Davis in Theoretical and Computational Fluid Dynamics

    Article 26 May 2022
    

12. Asymmetry of a Flow Which is Due to the Interaction of a Compression Shock with the Boundary Layer on a Longitudinally Ribbed Surface

    Numerical investigations of the asymmetry of a fluid flow in the channel of an air intake which is due to the interaction of a compression shock,...

    I. I. Mazhul’ in Journal of Engineering Physics and Thermophysics

    Article 01 July 2023

13. Numerical studies on uncontrolled and controlled shock wave/boundary layer interactions in hypersonic intake

    Understanding the phenomenon of Shock Wave/Boundary Layer Interaction (SBLI) is critical in develo** hypersonic aircraft as it is associated with...

    Dorbala Sai Naga Bharghava, Amit Krishnat Mali, ... Mrinal Kaushik in Aerospace Systems

    Article 31 October 2023
    

14. Shock-Wave/Boundary-Layer Interactions in Scramjet Intakes with Axisymmetric and Planar Isolators

    The present study numerically investigates the shock-wave/boundary-layer interactions (SWBLIs) inside a scramjet intake at Mach 4.03. A 2D-planar and...

    S. Sharath, Tamal Jana, Mrinal Kaushik in Advances in Astronautics Science and Technology

    Article 11 December 2023
    

15. Numerical studies on weak and strong ignition induced by reflected shock and boundary layer interaction

    In shock tube experiments, the interaction between the reflected shock and boundary layer can induce shock bifurcation and weak ignition. The weak...

    Chengyang Huang, Yuan Wang, ... Zheng Chen in Acta Mechanica Sinica

    Article 07 January 2022

16. Mach number effects on shock-boundary layer interactions over curved surfaces of supersonic turbine cascades

    The effects of inlet Mach number on the unsteadiness of shock-boundary layer interactions (SBLIs) over curved surfaces are investigated for a...

    Hugo F. S. Lui, William R. Wolf, ... Datta V. Gaitonde in Theoretical and Computational Fluid Dynamics

    Article 11 July 2024
    

17. Nozzle geometry effects on supersonic wind tunnel studies of shock–boundary-layer interactions

    Many supersonic wind tunnel experiments investigate shock–boundary-layer interactions by measuring the response of tunnel wall boundary layers to an...

    Kshitij Sabnis, Daniel S. Galbraith, ... John A. Benek in Experiments in Fluids

    Article Open access 17 December 2022
    

18. Numerical simulation of noise generated by shock (wave) and boundary layer interaction in aero-engine inlet

    We utilize the nonlinear acoustic solver (NLAS) and Ffowcs-Williams/Hawkings (FW-H) equation to investigate the noise generation and radiation due to...

    Yuanjun Dai, Yiran An, ... Qunfeng Zhang in Acta Mechanica Sinica

    Article 17 February 2022

19. Vibration Reduction of a Compliant Panel Under Ramp-Induced Shock Wave/Boundary Layer Interaction Through Aeroelastic Tailoring

    Experiments are performed in a Mach 2 wind tunnel to investigate the vibration of a compliant panel under a ramp-induced shock wave/boundary layer...

    Marc A. Eitner, Yoo-** Ahn, ... Noel T. Clemens in Topics in Modal Analysis & Parameter Identification, Volume 8

    Conference paper 2023
    

20. Hybrid LES/RANS Simulation of Shock/Turbulent Boundary-Layer Interactions

    In order to reduce the computational cost of Large Eddy Simulation method at high Reynolds number, the hybrid LES/RANS model-Improved Delayed...

    Tingkai Dai, Bo Zhang in Proceedings of the International Conference on Aerospace System Science and Engineering 2022

    Conference paper 2023