New Step Response Formulation for Inverse Heat Conduction
Effect of Passive Bleeding on Flow Structure over a Nonslender Delta Wing
Development of a URDF file for simulation and programming of a delta robot using ROS
Optimal Design of Annular Fin Shapes with Temperature-Dependent Properties
Cross Correlation and Inverse Heat Conduction by a Calibration Method
Survey of Station-Keeping Techniques for Libration Point Orbits
Effects of Reynolds Numbers on Wing Rock Induced by Forebody Vortices
Turbulent Mixing Simulation via a Quantum Algorithm
Enhanced Maneuverability of a Delta-Canard Combat Aircraft by Vortex Flow Control
Touch sensitive curved and flexible displays
Experimental study of the vortex flow and aerodynamic characteristics of a reverse delta wing
Numerical study of aerodynamic forces and flow physics of a delta wing in dynamic ground effect
Computational investigation of the flow structure over a pitching delta wing at supersonic speeds
Effects of pitch, yaw, and roll on delta wing skin friction topology
Analytic Steady-State Accuracy of a Three-Axis Spacecraft Attitude Estimator
Digital Control Algorithm Based on Delta-Operator for High-Frequency DC-DC Switching Converters
Optimal Combination of Magnetic Attitude Control with Impulsive Thrusting
Quadratically Constrained Least Squares with Aerospace Applications
Vector Wave Equation of Aeroacoustics and Acoustic Velocity Formulations for Quadrupole Source
Flow Stability Model of Centrifugal Compressors Based on Eigenvalue Approach
Diffusion Penetration Time for Transient Heat Conduction
Transonic Numerical and Experimental Evaluation of Unconventional Lambda Wing Control Surfaces
Effect of Dorsal Fin on Symmetry of Vortices over Slender Delta Wing
Numerical Investigations of Vortical Flow on Swept Wings with Round Leading Edges
Submerged Inlet Performance Enhancement Using a Unique Bump-Shaped Vortex Generator
Imaging of Broadband Noise from Rotating Sources in Uniform Axial Flow
Three-Dimensional Aircraft Conflict Resolution Based on Smoothing Methods
Orion Exploration Flight Test 1 (EFT-1) Best Estimated Trajectory Development
Canard flow improvement in a split canard configuration
DDES study of the aerodynamic forces and flow physics of a delta wing in static ground effect
Summary and Statistical Analysis of the First AIAA Sonic Boom Prediction Workshop
Vortex flow hypothesis for a yawed rotor blade in reverse flow*
Multiple model adaptive control using second level adaptation for a delta-wing aircraft