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Aerodynamic Coefficients of a 70-deg Spherecone in Hypersonic Flow
Development of Aerodynamic Loads Databases for the Space Launch System Booster Separation Event
Experimental Characterization of the Space Launch System Block 1B Liftoff and Transition Environment
Unsteady Surface Pressures on the SLS Block 1B Cargo Liftoff Configuration
AeroFusion: Data Fusion and Uncertainty Quantification for Entry Vehicles
Wind Tunnel Testing of Static Aerodynamic and Power Consumption Characteristics of an Octocopter
Ongoing Aeroelastic Prediction and Validation Activities at NASA Langley Research Center
Aerodynamic Implications of Aerocapture Systems for Uranus Orbiters
Post-Flight Aerodynamics Assessment of the Artemis-I Booster Separation Event
Application of the CATNLF Design Method to a Transonic Transport Empennage Using CDISC
Ongoing Subsonic Aeroelastic Optimization Research at NASA LaRC, Aeroelasticity Branch
Aeroelastic Analysis of Highly Flexible Wings with Linearized Frequency-Domain Aerodynamics
Unsteady Surface Pressures on the Space Launch System Block 1B Cargo Liftoff Configuration
Summary of the First AIAA Stability and Control Prediction Workshop
Flight Dynamics Research Facility - Perspective on Future Impacts
NASA Langley FUN3D Analyses in Support of the 1st AIAA Stability and Control Prediction Workshop
Program Overview: Vortex Interaction Aerodynamics Relevant to Military Air Vehicle Performance
Program Overview: Vortex Interaction Aerodynamics Relevant to Military Air Vehicle Performance
Predicting High-Lift Aerodynamics on NASA Common Research Model
NASA Langley FUN3D Analyses in Support of the 1st AIAA Stability and Control Prediction Workshop
NASA’s Quiet Electric ENgines (QUEEN): Summary of the QUEEN V2 Test
Evaluation of CFD for Simulation of High-Supersonic Control Surface Effectiveness
Computational Analysis of a Multiple-Nozzle Supersonic Retropropulsion Configuration
Gradient-Enhanced Reliability Analysis of Transonic Aeroelastic Flutter
Aeroelastic Analysis of Mach 0.8 Transonic Truss-Braced Wing Aircraft
Aeroservoelastic Modeling of Body Freedom Flutter for Control System Design
Aeroservoelastic Modeling of Body Freedom Flutter for Control System Design
Aeroservoelastic Modeling of Body Freedom Flutter for Control System Design
Toward Aerodynamic Shape Optimization for the Design of Natural-Laminar-Flow Wings
Topology Optimization of Low-Speed Aeroelastic Wind Tunnel Models
Exploring the Accuracy of RANS Simulations for Mars Entry Vehicles
Aerodynamics and Performance Flight Research and Airworthiness Best Practices
Exploration of Design Drivers for the RVLT Lift+Cruise Reference Aircraft