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UNS3D Near-Field Predictions for the Third AIAA Sonic Boom Prediction Workshop. 59:595-611. 2022
Wind Tunnel Experiment of Microjet-Based Flow Control on a Two-Dimensional Wing with Flap. 60:1-4. 2022
Design of Shape-Adaptive Deployable Slat-Cove Filler for Airframe Noise Reduction. 58:1034-1050. 2021
Open-Loop Linear Model Identification of aMultirotor Vehicle with Active Feedback Control. 57:1044-1061. 2020
Modal Identification of Aerodynamic Models for Spanwise Lift Distribution Control. 57:664-677. 2020
Structurally Consistent Class/Shape Transformation Equations for Morphing Airfoils. 56:505-516. 2019
Role of Blade Flexibility on Cycloidal Rotor Hover Performance. 55:1-19. 2018
Effects of Asymmetric Blade-Pitching Kinematics on Forward-Flight Performance of a Micro-Air-Vehicle-Scale Cycloidal-Rotor. 53:1568-1573. 2016
Hover Performance of a Small-Scale Helicopter Rotor for Flying on Mars. 53:1160-1167. 2016
Identification of Flight Dynamics of a Cylcocopter Micro Air Vehicle in Hover. 52:116-129. 2015
Design of an Infinite-Swept-Wing Glove for In-Flight Discrete-Roughness-Element Experiment. 51:1618-1631. 2014
Numerical Investigation of Actively Cooled Structures in Hypersonic Flow. 51:1522-1531. 2014
Transonic Aeroelastic Instability Suppression for a Swept Wing by Targeted Energy Transfer. 51:1467-1482. 2014
Development of a Micro Twin-Rotor Cyclocopter Capable of Autonomous Hover. 51:672-676. 2014
Effect of Rotor Geometry and Blade Kinematics on Cycloidal Rotor Hover Performance. 50:1340-1352. 2013
Adjoint-Based Aerodynamic Optimization of Supersonic Biplane Airfoils. 49:802-814. 2012
Testing and System Identification of an Ornithopter in Longitudinal Flight. 48:660-667. 2011
Improving the Aerodynamic Performance of Micro-Air-Vehicle-Scale Cycloidal Rotor: An Experimental Approach. 47:1117-1125. 2010
Aerodynamic-Structural Design Studies of Low-Sweep Transonic Wings. 47:505-514. 2010
Computational Study of Flexible Wing Ornithopter Flight. 46:2016-2031. 2009
In Pursuit of Grid Convergence, Part I: Two-Dimensional Euler Solutions. 47:1152-1166. 2009
Structural Analysis and Testing of an Ultralight Unmanned-Aerial-Vehicle Carbon-Composite Wing. 46:814-820. 2009
Design of Adjoint Based Laws for Wing Flutter Control. 48:331-335. 2009
Residual-Strength Assessment of Modified Transport Aircraft Fuselages. 46:85-94. 2009
Comparative Study of 3D Wing Drag Minimization by Different Optimization Techniques. 46:526-541. 2008
Optimum Shape Design for Unsteady Three-Dimensional Viscous Flows Using a Nonlinear Frequency-Domain Method. 44:1513-1527. 2007
Improving aircraft sequencing and separation at a small aircraft transportation system airport. 43:1636-1642. 2006
Introduction: Small aircraft transportation system high volume operations. 43:1601-1601. 2006
Modeling Mechanical Fasteners in Single-Shear Lap Joints. 41:1491-1497. 2004
Multi-Element High-Lift Configuration Design Optimization Using Viscous Continuous Adjoint Method. 41:1082-1097. 2004
Bodies Having Minimum Pressure Drag in Supersonic Flow: Investigating Nonlinear Effects. 47:1451-1454. 2004
Comparison of Residual Strength Estimates for Bolted Lap-Joint Panels. 41:657-664. 2004
Linkup Strength of 2024-T3 Bolted Lap Joint Panels with Multiple Site Damage. 41:359-364. 2004
Nonlinear Aeroelasticity. 40:857-874. 2003
Sonic Boom Alleviation Using Keel Configurations. 40:363-369. 2003
Computational and experimental investigation of limit cycle oscillations of nonlinear aeroelastic systems. 39:133-141. 2002
Constrained Multipoint Aerodynamic Shape Optimization Using an Adjoint Formulation and Parallel Computers, Part 1. 36:51-60. 1999
Re-Engineering the Design Process Through Computation. 36:36-50. 1999
Aeroelastic response of a rigid wing supported by nonlinear springs. 35:616-622. 1998
Constrained multipoint aerodynamic shape optimization using an adjoint formulation and parallel computers. 36:61-74. 1997
Flow about a slotted cylinder-airfoil combination in a wind tunnel. 33:716-721. 1996
Aeroelastic behavior of composite plates subject to damage growth. 33:68-73. 1996
Experiments and analysis for a gust generator in a wind tunnel. 33:139-148. 1996
Measurement and improvement of the lateral agility of the F-18. 30:803-804. 1993
Fighter agility metrics, research and test. 29:452-457. 1992
Efficient method for computing transonic and supersonic flows about aircraft. 27:223-231. 1990
Euler equation simulation of propeller-wing interaction in transonicflow. 21:835-839. 1984
COMPARISON OF MODEL HELICOPTER ROTOR PRIMARY AND SECONDARY BLADE VORTEX INTERACTION BLADE SLAP. 21:346-350. 1984
Structural modification to achieve antiresonance in helicopters. 19:499-504. 1982
Transonic Flow Calculations for a Wing in a Wind Tunnel. 18:707-711. 1981
Finite-volume solutions to the Euler equations in transonic flow. 20:127-133. 1981
Computational Investigation of Step Excrescence Sensitivity in a Swept-Wing Boundary Layer 2017
Unsteady Aerodynamic Model Based on the Leading-Edge Stagnation Point 2016
Experimental and Computational Analysis of Rigid Flapping Wings for Micro Air Vehicles 2015
Computational Evaluation and Linear Stability of a Transonic Laminar-Flow Wing Glove 2015
Computations of High-Lift Wing Configuration on Unstructured Grids Using k-omega Models 2013
Understanding Micro Air Vehicle Flapping-Wing Aerodynamics Using Force and Flowfield Measurements 2013
Complete Computational Fluid Dynamics Analysis of Velocity XL with Flight-Test Verification 2012
Parallel Multigrid Algorithm for Aeroelasticity Simulations 2010
Computational Study of Flexible Wing Ornithopter Flight 2009
Mesh Generation and Deformation Algorithm for Aeroelasticity Simulations 2008
Nonlinear Aeroelasticity 2003
Computational and experimental investigation of limit cycle oscillations of nonlinear aeroelastic systems 2002