Predictive Control Design for an Unmanned Aerial Vehicle
Evaluation of Heat Pipes in the Temperature Range of 450 to 700 K
F-22 Aeroelastic Design and Test Validation AIAA Paper 2007-1764 CD-ROM Number 7
Spatial approaches to moons from resonance relative to invariant manifolds
Loop Heat Pipe Radiator Trade Study for the 300-550 K Temperature Range
Safety Enhancements Available by Converting MSG-2 Aircraft Maintenance Programs to MSG-3
A Dynamical Systems Analysis of Resonant Flybys: Ballistic Case
A Dynamical Systems Analysis of Resonant Flybys: Ballistic Case
Fuel Injection Strategies to Increase Full-Load Torque Output of a Direct-Injection SI Engine
Dynamical Systems Analysis of Planetary Flybys and Approach: Planar Europa Orbiter
Spark Anemometry of Bulk Gas Velocity at the Plug Gap of a Firing Engine
Finite-Element Solutions for Turbulent Flow over the NACA 0012 Airfoil (Invited) (AIAA 2015-1531)
Shore-Based Reference Facility (SRF) Requirements for Platform Management Systems
Thermo-Physical Properties of Intermediate Temperature Heat Pipe Fluids
Water Heat Pipe Radiator Trade Study for the 300-550 K Temperature Range
Relaxation spectra of asphalt binders and the Christensen–Anderson rheological model
Hybrid Transmission Line for ECRH in the Helically Symmetric Experiment
Equilibrium and stability of a circularly towed cable subject to aerodynamic drag
AIAA-2004-5084 F/A-22 High Angle of Attack Buffet - Test Adequacy Analysis
Launches and the environment: Lessons learned.
AIAA-2004-1678 Low Speed Wind Tunnel Buffet Testing on the F/A-22