Ablation Analyses of Optimized Nose Tips for Hypersonic Vehicles
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 and Efficient Model Predictive Control for Booster Reentry
Adaptive Attitude Tracking Control Preserving the Self-Reduction Property
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
Aerothermodynamic Study of Ultrahigh-Temperature Ceramic Winglet for Atmospheric Reentry Test
AIAA Policy Statements and Manuscript Review Process
AIAA Policy Statements and Manuscript Review Process
AIAA Policy Statements and Manuscript Review Process
AIAA Policy Statements and Manuscript Review Process
AIAA Policy Statements and Manuscript Review Process
AIAA Policy Statements and Manuscript Review Process
AIAA Policy Statements and Manuscript Review Process
AIAA Policy Statements and Manuscript Review Process
AIAA Policy Statements and Manuscript Review Process
AIAA Policy Statements and Manuscript Review Process
AIAA Policy Statements and Manuscript Review Process
AIAA Policy Statements and Manuscript Review Process
AIAA Policy Statements and Manuscript Review Process
Alternative Aerodynamic Uncertainty Modeling Approaches for Flutter Reliability Analysis
Ambiguous Orbits in Elliptic Chief Spacecraft Relative Orbit Estimation with Range-Only Measurements
Analyses for the Second Aeroelastic Prediction Workshop Using the EZNSS Code
Analysis and Optimization of Double-Jet Film-Cooling Holes
Analysis of Local Stress Ratio for Delamination in Composites Under Fatigue Loads
Analysis of the CanX-1 Engineering Model Spectral Reflectance Measurements
Analysis of Turbulence Model Uncertainty for Shock-Wave/Boundary-Layer Interaction Simulations
Analysis of Two-Impulse Capture Trajectories into Halo Orbits of Sun–Mars System
Analysis on Propulsive Performance of Hollow Rotating Detonation Engine with Laval Nozzle
Analytical Approach on Buckling Mode and Critical Stress of Composite Sandwich Shells
Analytical Sensitivities of Principal Components in Time-Series Analysis of Dynamical Systems
Analytic Free-Molecular Aerodynamics for Rapid Propagation of Resident Space Objects