Flutter Analysis with Stabilized Finite Elements Based on the Linearized Frequency-Domain Approach
Efficient Basis Derivatives Evaluations for High-order Discontinuous Galerkin Schemes
Numerical Modeling of Helium Bubbling in a Cryogenic Propellant Tank
Predicting Quadcopter Noise With The Lattice-Boltzmann Method
US Side Magnetic Nozzle Computational Modeling Efforts Update Cont.
Node Ordering for Stabilizing Preconditioners Based on Incomplete LU Decomposition
MXMC: Generalized Multi-Model Monte Carlo Simulation for Uncertainty Propagation
Statistical Approach on Utilizing Ground-based Experiments to Model Break-up Events
Impact of Analytic Derivatives on Optimization of N-Impulse Orbit Transfer
Numerical Investigation of Roughness Effects on Transition on Spherical Capsules
Verification of Anisotropic Mesh Adaptation for Turbulent Simulations over ONERA M6 Wing
Modeling Meteoroid Densities for Spacecraft Risk Assessment
Summary of the 1st AIAA Geometry and Mesh Generation Workshop (GMGW-1) and Future Plans
Predictive Lateral Logic for Numerical Entry Guidance Algorithms
Jig-Shape Optimization of a Low-Boom Supersonic Aircraft
Computational Aerothermodynamic Environments for the Mars 2020 Entry Capsule
Numerical Simulation of a Complete Low-Speed Wind Tunnel Circuit
A Nonlinear Viscoelastic-Viscoplastic Constitutive Model for Epoxy Polymers
Open Rotor Computational Aeroacoustic Analysis with an Immersed Boundary Method
Numerical CFD Simulation and Test Correlation in a Flight Project Environment
Numerical CFD Simulation and Test Correlation in a Flight Project Environment
Least-Squares Adaptive Control Using Chebyshev Orthogonal Polynomials
Efficient Preconditioning of a High-Order Solver for Multiple Physics
Overview of Human Thermal Modeling, Thermoregulation, and Thermal Comfort at NASA
FUN3D Overview Part IV: Turbulence Model Discretization
A Mathematical Analysis of Conflict Prevention Information
A review on the response of blast loaded laminated composite plates
High Speed Solution of Spacecraft Trajectory Problems Using Taylor Series Integration
Non-Linear System Identification for Aeroelastic Systems with Application to Experimental Data
Quickly Approximating the Distance Between Two Objects
Aerodynamic Model for Insect Flapping Wings with Induced Flow Effect
U or V Shape: Dissipation Effects on Cylinder Flow Implicit Large-Eddy Simulation
Remaining useful life estimation under degradation and shock damage