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Recent Improvements to the Copernicus Trajectory Design and Optimization System
FUN3D Analyses in Support of the 5th Propulsion Aerodynamics Workshop (PAW5) - Inlet Test Case
Summary of Results from the Third Aeroelastic Prediction Workshop Flight Test Working Group
Design of a Crossflow Attenuated Natural Laminar Flow Flight Test Article
FUN3D Analyses in Support of the 5th Propulsion Aerodynamics Workshop - Nozzle Test Case
USM3D-ME Revised SA-neg Implementation and Assessment for Seventh Drag Prediction Workshop Solutions
Aeroelastic Indicial Response Reduced-Order Modeling for Flexible Flight Vehicles
Comparison of Aerodynamic Analysis Tools Applied to a Propeller-Blown Wing
Kestrel Results for DPW-VII Including Adaptive Mesh and IDDES Computations
Summary of Results from the Third Aeroelastic Prediction Workshop Flight Test Working Group
Optimal Aircraft Control Surface Layouts for Maneuver and Gust Load Alleviation
Nearfield Summary and Statistical Analysis of the Second AIAA Sonic Boom PredictionWorkshop
Optimizing Proprotor Blades Using Coupled Aeroacoustic and Aerodynamic Sensitivities
Effects of Spatial Resolution on Retropropulsion Aerodynamics in an Atmospheric Environment
Aeroelastic Analysis of Highly Flexible Wings with Linearized Frequency-Domain Aerodynamics
Dragonfly Entry and Descent Flight Mechanics Modeling and Analysis
Comparison of Aerodynamic Analysis Tools Applied to a Propeller-Blown Wing
AePW-3 High Angle Working Group Test Case Selection and Data Submission
Linear Analysis of a Two-Parachute System Undergoing Pendulum Motion
Investigation of Reduced-Order Modeling for Aircraft Stability and Control Prediction
FUN3D and USM3D Analysis of the 4th AIAA Propulsion Aerodynamics Workshop Nozzle Test Case
FUN3D and USM3D Analysis of the Propulsion Aerodynamic Workshop 2018 S-Duct Test Case
NASA Langley FUN3D Analyses in Support of the 1st AIAA Stability and Control Prediction Workshop
Effect of Ice Shape Fidelity on Swept-Wing Aerodynamic Performance
FUN3D Analyses in Support of the 1st AIAA Stability and Control Prediction Workshop
IFCPT S-Duct Grid-Adapted FUN3D Computations for the Third Propulsion Aerodynamics Works
Application of Exactly Linearized Error Transport Equations to AIAA CFD Prediction Workshops
NASA Langley FUN3D Analyses in Support of the 1st AIAA Stability and Control Prediction Workshop
Summary of the First AIAA Stability and Control Prediction Workshop
Progress and Plans for the 2nd Aeroelastic Prediction Workshop (AePW-2)
Wall-Resolved Large-Eddy Simulations of Transonic Shock-Induced Flow Separation
The NASA High Speed ASE Project: Computational Analyses of a Low-Boom Supersonic Configuration
Aeroelastic Uncertainty Quantification Studies Using the S4T Wind Tunnel Model
Computational and Experimental Study of Supersonic Nozzle Flow and Shock Interactions
A Status Review of the Commercial Supersonic Technology (CST) Aeroservoelasticity (ASE) Project