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Effects of Surface Compliance on Shock Boundary Layer Interaction in the Caltech Mach 4 Ludwieg Tube
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What this work says
Outgoing claims: the papers this work cites, builds on, or argues with.
inferredcites →https://doi.org/10.1016/j.jsv.2018.11.035openalex-snapshot
Exploring the response of a thin, flexible panel to shock-turbulent boundary-layer interactions
inferredcites →https://doi.org/10.1115/1.3153712openalex-snapshot
Formulas for Natural Frequency and Mode Shape
inferredcites →https://doi.org/10.21236/ada049535openalex-snapshot
Laminar Boundary Layer Stability Measurements at Mach 7 Including Wall Temperature Effects
inferredcites →https://doi.org/10.2514/6.2013-2016openalex-snapshot
Full-field, dynamic pressure and displacement measurements of a panel excited by shock boundary-layer interaction
inferredcites →https://doi.org/10.2514/6.2015-0530openalex-snapshot
Pulsed Laser Diode for Use as a Light Source for Short-Exposure, High-Frame-Rate Flow Visualization
inferredcites →https://doi.org/10.2514/6.2016-1088openalex-snapshot
Measurement and simulation of hypersonic fluid-structural interaction on a cantilevered plate in a Mach 6 flow
inferredcites →https://doi.org/10.2514/6.2017-0402openalex-snapshot
Fluid-Structure Interactions on a Slender Cone under Quiet Flow Conditions at Mach 6
inferredcites →https://doi.org/10.7907/z93x84m6openalex-snapshot
On the Stability of Supersonic Boundary Layers with Injection
What points at this work
Incoming claims: where this work appears in other papers’ reference lists and arguments.
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Measurements of Panel Vibration with DIC and LDV Imaged Through a Mach 5 Flow
inferred← citeshttps://doi.org/10.1007/s00348-021-03314-4openalex-snapshot
Methodology to image the panel surface pressure power spectra in weakly coupled fluid/structure interactions
inferred← citeshttps://doi.org/10.1007/s00348-022-03551-1openalex-snapshot
Characterization of shock-induced panel flutter with simultaneous use of DIC and PIV
inferred← citeshttps://doi.org/10.1007/s00348-022-03559-7openalex-snapshot
Unsteadiness in hypersonic leading-edge separation
inferred← citeshttps://doi.org/10.1007/s11071-024-10108-wopenalex-snapshot
Nonlinear aeroelastic behavior of a panel impinged by oscillating shock
inferred← citeshttps://doi.org/10.1007/s40799-020-00393-6openalex-snapshot
Modal Parameter Estimation of a Compliant Panel Using Phase-based Motion Magnification and Stereoscopic Digital Image Correlation
inferred← citeshttps://doi.org/10.1016/j.cam.2023.115401openalex-snapshot
Numerical study of the effect of micro vortices on chaotic flutter
inferred← citeshttps://doi.org/10.1016/j.euromechflu.2021.07.002openalex-snapshot
Spatially developing supersonic turbulent boundary layer subjected to static surface deformations
inferred← citeshttps://doi.org/10.1016/j.jfluidstructs.2022.103660openalex-snapshot
Dynamic interaction between shock wave turbulent boundary layer and flexible panel
inferred← citeshttps://doi.org/10.1016/j.jfluidstructs.2023.103894openalex-snapshot
Vibration of a thin panel exposed to ramp-induced shock-boundary layer interaction at Mach 2
inferred← citeshttps://doi.org/10.1016/j.jfluidstructs.2025.104271openalex-snapshot
Assessment of Aeroelastic Coupling between a Shock Boundary Layer Interaction and a Flexible Panel
inferred← citeshttps://doi.org/10.1016/j.jfluidstructs.2026.104564openalex-snapshot
Turbulent shock-wave boundary layer interactions over compliant panels: Insights from one-way analyses
inferred← citeshttps://doi.org/10.1017/flo.2022.28openalex-snapshot
Fluid–structural coupling of an impinging shock–turbulent boundary layer interaction at Mach 3 over a flexible panel
inferred← citeshttps://doi.org/10.1063/5.0172475openalex-snapshot
High-speed shock–boundary-layer interaction over deformed surfaces
inferred← citeshttps://doi.org/10.1063/5.0175161openalex-snapshot
Aeroelastic response of a thin panel excited by a separated shock–boundary layer interaction
inferred← citeshttps://doi.org/10.1063/5.0179082openalex-snapshot
Shock-wave/turbulent boundary-layer interaction with a flexible panel
inferred← citeshttps://doi.org/10.1109/access.2024.3430219openalex-snapshot
Optical Fiber Bragg Grating-Based Measurement of Fluid-Structure Interaction on a Cantilever Panel in High-Speed Flow
inferred← citeshttps://doi.org/10.1146/annurev-fluid-120720-022542openalex-snapshot
Dynamics of Three-Dimensional Shock-Wave/Boundary-Layer Interactions
inferred← citeshttps://doi.org/10.1364/ao.457151openalex-snapshot
Methodology of designing compact schlieren systems using off-axis parabolic mirrors
inferred← citeshttps://doi.org/10.2514/1.j060114openalex-snapshot
Experiments on a Thin Panel Excited by Turbulent Flow and Shock/Boundary-Layer Interactions
inferred← citeshttps://doi.org/10.2514/1.j061886openalex-snapshot
High-Speed Fluid-Structure Interactions on a Compliant Panel Under Shock Impingement
inferred← citeshttps://doi.org/10.2514/1.j063554openalex-snapshot
Panel Aeroelastic Hysteresis Induced by Shock-Reflection Transition
inferred← citeshttps://doi.org/10.2514/1.j063702openalex-snapshot
Aeroacoustic Loading of Impinging Supersonic Boundary-Layer Interaction on Statically Deformed Surfaces
inferred← citeshttps://doi.org/10.2514/1.j064083openalex-snapshot
Fluid-Structure Interactions of a Fin over a Compliant Panel in Supersonic Flow
inferred← citeshttps://doi.org/10.2514/1.j064183openalex-snapshot
Flow Response of a Laminar Shock–Boundary Layer Interaction to Prescribed Surface Motions
inferred← citeshttps://doi.org/10.2514/1.j064575openalex-snapshot
Aeroelastic Effects in Supersonic Shock-Turbulent Boundary Layer Interaction over Flexible Panels
inferred← citeshttps://doi.org/10.2514/1.j066113openalex-snapshot
Nonlinear Aeroelastic Behavior of a Panel Subjected to Oscillating Shock Waves
inferred← citeshttps://doi.org/10.2514/6.2021-2493openalex-snapshot
Effect of Shock-Wave Boundary Layer Interaction on Vibratory Response of Compliant Panel
inferred← citeshttps://doi.org/10.2514/6.2022-2486openalex-snapshot
Effect of Structural Modifications on Vibratory Response of Panel under Ramp-Induced Shock Wave Boundary Layer Interaction
inferred← citeshttps://doi.org/10.2514/6.2022-3984openalex-snapshot
Low order analysis of panel vibration under ramp-induced shock / boundary layer interaction
inferred← citeshttps://doi.org/10.2514/6.2022-4136openalex-snapshot
Unsteadiness in Shock/Boundary-Layer Interaction Over a Compliant Panel at Mach 2
inferred← citeshttps://doi.org/10.2514/6.2023-0948openalex-snapshot
Design of Aerothermoelastic Experiments in the AFRL Mach 6 High Reynolds Number Facility
inferred← citeshttps://doi.org/10.2514/6.2023-3605openalex-snapshot
Measuring fluid structure interaction in a cantilevered panel using optical fiber Bragg Gratings
inferred← citeshttps://doi.org/10.2514/6.2024-1153openalex-snapshot
Experimental Investigation of an Impinging Shock-Boundary Layer Interaction on a Compliant Panel in Mach 4 Flow
inferred← citeshttps://doi.org/10.2514/6.2025-0415openalex-snapshot
Transitional Shock-Wave Boundary Layer Interaction of a Heated Cantilever
inferred← citeshttps://doi.org/10.2514/6.2025-1308openalex-snapshot
Experimental Study of the Fluid-Structure Interaction Induced by a Mach 5 Compression Ramp-SBLI
inferred← citeshttps://doi.org/10.2514/6.2026-2045openalex-snapshot
Mach 6 Aerothermoelastic Experiment for an Inclined, Compliant CFCF Panel With Buckling
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