☆ 4.7 Article

Separation length scaling for dual-incident shock wave-turbulent boundary layer interactions with different shock wave distances

JOURNAL OF FLUID MECHANICS (2023)

Related references

Note: Only part of the references are listed.

Article Engineering, Aerospace

Effects of Wall Temperature on Hypersonic Impinging Shock-Wave/Turbulent-Boundary-Layer Interactions

Feng-Yuan Zuo et al.

Summary: This study investigates the characteristics and effects of hypersonic impinging shock-wave/turbulent-boundary-layer interactions at different wall temperatures and Reynolds numbers through numerical simulation. The results show that RANS is capable of predicting the main features, and it is found that cooling the wall and increasing the Reynolds number will reduce the interaction zone.

AIAA JOURNAL (2022)

Add to Collection

Article Mechanics

Comparative study on single-incident and dual-incident shock wave/turbulent boundary layer interactions with identical total deflection angle

Xin Li et al.

Summary: This study investigates the interactions between the boundary layer and two successive incident shock waves in supersonic mixed-compression inlets. Experimental and analytical methods are used to study the turbulent boundary layer separation induced by single and dual shock waves. The study reveals different flow features and separation region shapes depending on the distance between the shock waves.

JOURNAL OF FLUID MECHANICS (2022)

Add to Collection

Article Mechanics

Momentum balance based model for predicting the scale of separation bubbles induced by incident shock wave/turbulent boundary layer interactions

Wen-Zhong Xie et al.

Summary: This study predicts shock wave/turbulent boundary layer interactions (SWTBLIs) using numerical methods and generates detailed flow field data. A model for predicting the scale of SWTBLI separation bubble is proposed based on momentum balance, and essential correlations for key physical quantities are provided. The experimental results confirm the accuracy of the model.

EUROPEAN JOURNAL OF MECHANICS B-FLUIDS (2022)

Add to Collection

Article Engineering, Aerospace

Scaling of interaction lengths for hypersonic shock wave/turbulent boundary layer interactions

Yuting Hong et al.

Summary: The study investigated the interaction length induced by Shock Wave/Turbulent Boundary-Layer Interactions (SWTBLIs) in hypersonic flow, identifying two scaling relationships based on different Reynolds numbers. This provides valuable guidelines for engineering prediction and enriches the knowledge of hypersonic SWTBLIs.

CHINESE JOURNAL OF AERONAUTICS (2021)

Add to Collection

Article Physics, Fluids & Plasmas

Scaling of hypersonic shock/turbulent boundary layer interactions

Clara M. Helm et al.

Summary: This paper examines a separation length scaling method for shock/turbulent boundary layer interactions, modifying existing methods to include heat transfer effects and evaluating it across a range of STBLI conditions. The results show a linear collapse of all incipiently separated STBLI data with the new generalized scaling method, while no collapse is observed for fully separated interactions.

PHYSICAL REVIEW FLUIDS (2021)

Add to Collection

Article Computer Science, Interdisciplinary Applications

Incident shock wave and supersonic turbulent boundarylayer interactions near an expansion corner

Fulin Tong et al.

COMPUTERS & FLUIDS (2020)

Add to Collection

Article Engineering, Mechanical

Scaling for steady and traveling shock wave/turbulent boundary layer interactions

P. S. R. Toure et al.

EXPERIMENTS IN FLUIDS (2020)

Add to Collection

Article Computer Science, Interdisciplinary Applications

Flow patterns of dual-incident shock waves/turbulent boundary layer interaction

Xin Li et al.

JOURNAL OF VISUALIZATION (2020)

Add to Collection

Article Mechanics

Low-frequency unsteadiness of shock-wave/boundary-layer interaction in an isolator with background waves

Ziao Wang et al.

PHYSICS OF FLUIDS (2020)

Add to Collection

Article Mechanics

Corner effects for oblique shock wave/turbulent boundary layer interactions in rectangular channels

X. Xiang et al.

JOURNAL OF FLUID MECHANICS (2019)

Add to Collection

Article Mechanics

Confinement effects on regular-irregular transition in shock-wave-boundary-layer interactions

Ilan J. Grossman et al.

JOURNAL OF FLUID MECHANICS (2018)

Add to Collection

Article Mechanics

Oscillation of the shock train in an isolator with incident shocks

Nan Li et al.

PHYSICS OF FLUIDS (2018)

Add to Collection

Article Engineering, Aerospace

Unthrottled Flows with Complex Background Waves in Curved Isolators

He-xia Huang et al.

AIAA JOURNAL (2017)

Add to Collection

Article Mechanics

Evolution of supersonic corner vortex in a hypersonic inlet/isolator model

He-Xia Huang et al.

PHYSICS OF FLUIDS (2016)

Add to Collection

Article Engineering, Aerospace

Experimental results on unsteady shock-wave/boundary-layer interaction induced by an impinging shock

Dennis Daub et al.

CEAS SPACE JOURNAL (2016)

Add to Collection

Article Mechanics

On the transition between regular and irregular shock patterns of shock-wave/boundary-layer interactions

Jan Matheis et al.

JOURNAL OF FLUID MECHANICS (2015)

Add to Collection

Article Mechanics

Numerical study of oblique shock-wave/boundary-layer interaction considering sidewall effects

Bo Wang et al.

JOURNAL OF FLUID MECHANICS (2015)

Add to Collection

Review Engineering, Aerospace

Progress in shock wave/boundary layer interactions

Datta V. Gaitonde

PROGRESS IN AEROSPACE SCIENCES (2015)

Add to Collection

Article Engineering, Aerospace

Length Scales and Time Scales of a Heated Shock-Wave/Boundary-Layer Interaction

V. Jaunet et al.

AIAA JOURNAL (2014)

Add to Collection

Review Mechanics

Low-Frequency Unsteadiness of Shock Wave/Turbulent Boundary Layer Interactions

Noel T. Clemens et al.

ANNUAL REVIEW OF FLUID MECHANICS, VOL 46 (2014)

Add to Collection

Article Mechanics

Confinement effects in shock wave/turbulent boundary layer interactions through wall-modelled large-eddy simulations

Ivan Bermejo-Moreno et al.

JOURNAL OF FLUID MECHANICS (2014)

Add to Collection

Article Mechanics

A scaling analysis for turbulent shock-wave/boundary-layer interactions

L. J. Souverein et al.

JOURNAL OF FLUID MECHANICS (2013)

Add to Collection

Article Engineering, Mechanical

Behavior of shock trains in a hypersonic inlet/isolator model with complex background waves

H. J. Tan et al.

EXPERIMENTS IN FLUIDS (2012)

Add to Collection

Article Mechanics

Low-frequency unsteadiness in shock wave-turbulent boundary layer interaction

Stephan Priebe et al.

JOURNAL OF FLUID MECHANICS (2012)

Add to Collection

Article Engineering, Aerospace

Direct Numerical Simulation Database for Impinging Shock Wave/Turbulent Boundary-Layer Interaction

Sergio Pirozzoli et al.

AIAA JOURNAL (2011)

Add to Collection

Article Engineering, Aerospace

Shock-Wave/Boundary-Layer Interactions in a Model Scramjet Intake

L. Krishnan et al.

AIAA JOURNAL (2009)

Add to Collection

Article Engineering, Aerospace

Direct Numerical Simulation of a Reflected-Shock-Wave/Turbulent-Boundary-Layer Interaction

S. Priebe et al.

AIAA JOURNAL (2009)

Add to Collection

Article Mechanics

Three-dimensional instantaneous structure of a shock wave/turbulent boundary layer interaction

R. A. Humble et al.

JOURNAL OF FLUID MECHANICS (2009)

Add to Collection

Article Mechanics

Unsteady aspects of an incident shock wave/turbulent boundary layer interaction

R. A. Humble et al.

JOURNAL OF FLUID MECHANICS (2009)

Add to Collection

Article Mechanics

Some physical aspects of shock wave/boundary layer interactions

Jean Delery et al.

SHOCK WAVES (2009)

Add to Collection

Article Mechanics

SBLI control for wings and inlets

Holger Babinsky et al.

SHOCK WAVES (2008)

Add to Collection

Article Engineering, Aerospace

Direct numerical simulation of supersonic turbulent boundary layer over a compression ramp

M. Wu et al.

AIAA JOURNAL (2007)

Add to Collection

Article Mechanics

Direct numerical simulation of impinging shock wave/turbulent boundary layer interaction at M=2.25

Sergio Pirozzoli et al.

PHYSICS OF FLUIDS (2006)

Add to Collection

Article Engineering, Aerospace

Correlations to predict the streamwise influence regions in supersonic turbulent flows

MD Ramesh et al.

JOURNAL OF AIRCRAFT (2004)

Add to Collection

Article Engineering, Aerospace

Fifty years of shock-wave/boundary-layer interaction research: What next?

DS Dolling

AIAA JOURNAL (2001)

Add to Collection

© Peeref 2019-2024. All rights reserved.