Absolute Nodal Coordinate Formulation-Based Shape Sensing Approach for Large Deformation: Plane Beam
Accurate and Robust Hybrid HLLC Riemann Solver on Triangular Grids
Acoustic Effects of Liner Damage on Zero-Splice Turbofan Intake Liners: Computational Study
Acquisition of a Desired Pure-Spin Condition for a Magnetically Actuated Spacecraft
Active Polynomial Chaos Expansion for Reliability-Based Design Optimization
Adaptable Recursive Update Filter
Adaptive Estimation and Control Algorithms for Certain Independent Control Axis Misalignments
Adjoint-Based Sensitivity Analysis for Airfoil Flow Control Aiming at Lift-to-Drag Ratio Improvement
Adjustment Method of Coupled Dual-Surface Accuracy for Antennas Using Interval Model Updating
Aerodynamic Design of Nozzles with Uniform Outflow for Hypervelocity Ground-Test Facilities
Aeroelastic Analysis of a Cycloidal Rotor Under Various Operating Conditions
Aeroelastic Systems with Softening Nonlinearity
Aeroelastic Wind-Tunnel Test for Aerodynamic Uncertainty Model Validation
Aeromechanics Analysis of a High-Advance-Ratio Lift-Offset Coaxial Rotor System
Aeromechanics of a Coaxial Ultralight Rotorcraft During Turn, Climb, and Descent Flight
Aerothermodynamic Analysis of High-Altitude Space Launcher with Direct-Simulation Monte Carlo Method
AIAA Policy Statements and Manuscript Review Process
AIAA Policy Statements and Manuscript Review Process