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Review of Output-Based Error Estimation and Mesh Adaptation in Computational Fluid Dynamics

AIAA journal, 2011-04, Vol.49 (4), p.673-694

2011

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Optimization of Dielectric Barrier Discharge Plasma Actuators for Active Aerodynamic Flow Control

AIAA journal, 2009-09, Vol.47 (9), p.2169-2178

2009

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Performance Variations of Leading-Edge Tubercles for Distinct Airfoil Profiles

AIAA journal, 2011-01, Vol.49 (1), p.185-194

2011

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Almost 40 Years of Airframe Noise Research: What Did We Achieve?

Journal of aircraft, 2010-03, Vol.47 (2), p.353-367

Dobrzynski, Werner

2010

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Hierarchical Kriging Model for Variable-Fidelity Surrogate Modeling

AIAA journal, 2012-09, Vol.50 (9), p.1885-1896

2012

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Improving variable-fidelity surrogate modeling via gradient-enhanced kriging and a generalized hybrid bridge function

Aerospace science and technology, 2013-03, Vol.25 (1), p.177-189

2013

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Separation Control with Nanosecond-Pulse-Driven Dielectric Barrier Discharge Plasma Actuators

AIAA journal, 2012-02, Vol.50 (2), p.350-365

2012

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Effects of Leading-Edge Protuberances on Airfoil Performance

AIAA journal, 2007-11, Vol.45 (11), p.2634-2642

2007

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Robust Flight Control Using Incremental Nonlinear Dynamic Inversion and Angular Acceleration Prediction

Journal of guidance, control, and dynamics, 2010-11, Vol.33 (6), p.1732-1742

2010

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Large-Eddy Simulation: Current Capabilities, Recommended Practices, and Future Research

AIAA journal, 2010-08, Vol.48 (8), p.1772-1784

2010

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Minimum-Landing-Error Powered-Descent Guidance for Mars Landing Using Convex Optimization

Journal of guidance, control, and dynamics, 2010-07, Vol.33 (4), p.1161-1171

2010

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Parametric Study of an Oscillating Airfoil in a Power-Extraction Regime

AIAA journal, 2008-06, Vol.46 (6), p.1318-1330

2008

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Nonlinear Robust Adaptive Control of Flexible Air-Breathing Hypersonic Vehicles

Journal of guidance, control, and dynamics, 2009-03, Vol.32 (2), p.402-417

2009

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Use of kriging models to approximate deterministic computer models

AIAA journal, 2005-04, Vol.43 (4), p.853-863

2005

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Wall-Pressure Spectral Model Including the Adverse Pressure Gradient Effects

AIAA journal, 2012-10, Vol.50 (10), p.2168-2179

2012

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Practical Techniques for Low-Thrust Trajectory Optimization with Homotopic Approach

Journal of guidance, control, and dynamics, 2012-01, Vol.35 (1), p.245-258

2012

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Green–Gauss/Weighted-Least-Squares Hybrid Gradient Reconstruction for Arbitrary Polyhedra Unstructured Grids

AIAA journal, 2013-11, Vol.51 (11), p.2740-2747

2013

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Parameter-Free Simple Low-Dissipation AUSM-Family Scheme for All Speeds

AIAA journal, 2011-08, Vol.49 (8), p.1693-1709

2011

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Guest Editorial for the TAES Special Section on Deep Learning for Radar Applications

IEEE transactions on aerospace and electronic systems, 2024-02, Vol.60 (1), p.4-7

2024

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Experimental and Numerical Investigation of Turbulence-Airfoil Noise Reduction Using Wavy Edges

AIAA journal, 2013-11, Vol.51 (11), p.2695-2713

2013

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Three-Electrode Plasma Synthetic Jet Actuator for High-Speed Flow Control

AIAA journal, 2014-04, Vol.52 (4), p.879-882

2014

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Finite-Time Attitude Stabilization for a Spacecraft Using Homogeneous Method

Journal of guidance, control, and dynamics, 2012-05, Vol.35 (3), p.740-748

2012

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Indirect Impact-Angle-Control Against Stationary Targets Using Biased Pure Proportional Navigation

Journal of guidance, control, and dynamics, 2012-03, Vol.35 (2), p.700-704

2012

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Intercept-Angle Guidance

Journal of guidance, control, and dynamics, 2011-03, Vol.34 (2), p.484-492

Shima, Tal

2011

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Indirect Robust Adaptive Fault -Tolerant Control for Attitude Tracking of Spacecraft

Journal of guidance, control, and dynamics, 2008-09, Vol.31 (5), p.1456-1463

2008

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Review of Output-Based Error Estimation and Mesh Adaptation in Computational Fluid Dynamics

Optimization of Dielectric Barrier Discharge Plasma Actuators for Active Aerodynamic Flow Control

Performance Variations of Leading-Edge Tubercles for Distinct Airfoil Profiles

Almost 40 Years of Airframe Noise Research: What Did We Achieve?

Hierarchical Kriging Model for Variable-Fidelity Surrogate Modeling

Improving variable-fidelity surrogate modeling via gradient-enhanced kriging and a generalized hybrid bridge function

Separation Control with Nanosecond-Pulse-Driven Dielectric Barrier Discharge Plasma Actuators

Effects of Leading-Edge Protuberances on Airfoil Performance

Robust Flight Control Using Incremental Nonlinear Dynamic Inversion and Angular Acceleration Prediction

Large-Eddy Simulation: Current Capabilities, Recommended Practices, and Future Research

Minimum-Landing-Error Powered-Descent Guidance for Mars Landing Using Convex Optimization

Parametric Study of an Oscillating Airfoil in a Power-Extraction Regime

Nonlinear Robust Adaptive Control of Flexible Air-Breathing Hypersonic Vehicles

Use of kriging models to approximate deterministic computer models

Wall-Pressure Spectral Model Including the Adverse Pressure Gradient Effects

Practical Techniques for Low-Thrust Trajectory Optimization with Homotopic Approach

Green–Gauss/Weighted-Least-Squares Hybrid Gradient Reconstruction for Arbitrary Polyhedra Unstructured Grids

Parameter-Free Simple Low-Dissipation AUSM-Family Scheme for All Speeds

Guest Editorial for the TAES Special Section on Deep Learning for Radar Applications

Experimental and Numerical Investigation of Turbulence-Airfoil Noise Reduction Using Wavy Edges

Three-Electrode Plasma Synthetic Jet Actuator for High-Speed Flow Control

Finite-Time Attitude Stabilization for a Spacecraft Using Homogeneous Method

Indirect Impact-Angle-Control Against Stationary Targets Using Biased Pure Proportional Navigation

Intercept-Angle Guidance

Indirect Robust Adaptive Fault -Tolerant Control for Attitude Tracking of Spacecraft

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