2024
2023
2022
[1]
Modal analysis of a shear layer in high-supersonic cavity flows using data-driven and operator-based resolvent analysis.
In Bulletin of the American Physical Society2022.
[2]
Geometric Design of Hypersonic Vehicles for Optimal Mission Performance with High-Fidelity Aerodynamic Models.
In Journal of Aircraft, pp. 1–13, 2022.
[3]
PIDGeuN: Graph Neural Network-Enabled Transient Dynamics Prediction of Networked Microgrids Through Full-Field Measurement.
In arXiv preprint arXiv:2204.08557, 2022.
[4]
Modularized Bilinear Koopman Operator for Modeling and Predicting Transients of Microgrids.
In arXiv preprint arXiv:2205.03214, 2022.
[5]
Study of fluid–thermal–structural interaction in high-temperature high-speed flow using multi-fidelity multi-variate surrogates.
In Journal of Fluids and Structures, vol. 113, p. 103682, 2022.
[6]
Reduced-Order Modeling of Ship Airwakes with Atmospheric Turbulence Effects using Dynamic Graph Networks.
In AIAA SCITECH 2022 Forum, p. 2533, 2022.
[7]
Koopman Operators for Bifurcation Analysis in Hypersonic Aerothermoelasticity.
In AIAA SCITECH 2022 Forum, p. 0655, 2022.
[8]
Physics-Infused Reduced Order Modeling of Hypersonic Aerothermal Loads for Aerothermoelastic Analysis.
In AIAA SCITECH 2022 Forum, p. 0989, 2022.
[9]
Geometric Design of Hypersonic Vehicles for Optimal Mission Performance using Machine Learning.
In AIAA SCITECH 2022 Forum, p. 1304, 2022.
[10]
An Experimental and Computational Correlation Study for Fluid-Thermal-Structural Interaction of a Control Surface in Hypersonic Flow.
In AIAA SCITECH 2022 Forum, p. 0291, 2022.
2021
[1]
Applications of Gaussian Process Regression in the Aero-Thermo-Servo-Elastic Analysis Towards Integrated Hypersonic Flight Dynamic Analysis.
In 2021 60th IEEE Conference on Decision and Control (CDC), pp. 6–15, 2021.
[2]
Resilience analysis of cyber-physical networked microgrids with communication latency.
In 2021 IEEE Power & Energy Society General Meeting (PESGM), pp. 1–5, 2021.
[3]
Multi-Variate Gaussian Process Regression for Angles-Only Initial Orbit Determination.
In AAS/AIAA Astrodynamics Specialist Conference, 2020, pp. 3077–3096, 2021.
[4]
Assessment of high-temperature effects on hypersonic aerothermoelastic analysis using multi-fidelity multi-variate surrogates.
In AIAA Scitech 2021 Forum, p. 1610, 2021.
[5]
Time-varying linear reduced order model for hypersonic aerothermoelastic analysis.
In AIAA Scitech 2021 Forum, p. 1706, 2021.
[6]
Expedient hypersonic aerothermal prediction for aerothermoelastic analysis via field inversion and machine learning.
In AIAA Scitech 2021 Forum, p. 1707, 2021.
[7]
Hypersonic Trajectory Optimization with High-Fidelity Aerothermodynamic Models.
In AIAA Scitech 2021 Forum, p. 0715, 2021.
[8]
Sparse Nonlinear System Identification for Hypersonic Aerothermoelastic Analysis with Stochastic Loads.
In AIAA Scitech 2021 Forum, p. 1609, 2021.
[9]
Numerical Investigation of Fluid-Thermal-Structural Interaction for a Control Surface in Hypersonic Flow.
In AIAA Scitech 2021 Forum, p. 0911, 2021.
[10]
Identifying HOPF bifurcations of networked microgrids induced by the integration of EV charging stations.
In 2021 IEEE Transportation Electrification Conference & Expo (ITEC), pp. 690–694, 2021.
2020
[1]
Impact of high-temperature effects on the aerothermoelastic behavior of composite skin panels in hypersonic flow.
In AIAA Scitech 2020 Forum, p. 0937, 2020.
[2]
An aerothermoelastic analysis framework with reduced-order modeling applied to composite panels in hypersonic flows.
In Journal of Fluids and Structures, vol. 94, 2020.
[3]
Multi-Objective Optimization Framework for Hypersonic Aerothermoelastic Scaling Laws and Its Application.
In AIAA Journal, vol. 58, no. 7, pp. 3250–3257, 2020.
2019
[1]
A Surrogate-Based Optimization Framework for Hypersonic Aerothermoelastic Scaling Laws with Application to Skin Panels.
In 16th Dynamics Specialists Conference, pp. 1–27, 2019.
[2]Development of a Hypersonic Aerothermoelastic Framework and Its Application to Flutter and Aerothermoelastic Scaling of Skin Panels, PhD thesis, 2019
[3]
A multi-objective optimization framework for hypersonic aerothermoelastic scaling laws and its application to skin panels.
In International Forum on Aeroelasticity and Structural Dynamicsno. 2019-143, , pp. 1–44, 2019.
2018
[1]
Aerothermoelastic Scaling Laws for Hypersonic Skin Panel Configurations with Arbitrary Flow Orientation.
In 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, pp. 1–23, 2018.
[2]
An Integrated Aerothermoelastic Analysis Framework With Application to Skin Panels.
In AIAA Journal, vol. 56, no. 11, pp. 4562–4581, 2018.
[3]
Aerothermoelastic Scaling Laws for Hypersonic Skin Panel Configurations with Arbitrary Flow Orientation.
In AIAA Journal, 2018.
[4]
Efficient Modeling of Fluid-Structure-Thermal Interaction in Hypersonic Flow.
In 58th Israel Annual Conference on Aerospace Sciences2018.
Before 2018
[1]
Efficient Reduced-Order Modeling for Skin Panels in Hypersonic Flow and Its Application to Generating Aerothermoelastic Scaling Laws.
In International Forum on Aeroelasticity and Structural Dynamics2017.
[2]
An Aerothermoelastic Analysis Framework Enhanced by Model Order Reduction With Applications.
In 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, pp. 1–19, 2017.
[3]
An Integrated Aerothermoelastic Analysis Framework for Predicting the Response of Composite Panels.
In 15th Dynamics Specialists Conference, pp. 1–37, 2016.