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Flight dynamics
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dynamics
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Aerodynamic Coefficients of a 70-deg Spherecone in Hypersonic Flow
Recent NASA Wind Tunnel Free-Flight Testing of a Multirotor Unmanned Aircraft System Vehicle
Aerodynamic Coefficients of a 70-deg Spherecone in Hypersonic Flow
FUN3D Analyses in Support of the 5th Propulsion Aerodynamics Workshop (PAW5) - Inlet Test Case
In search of data-driven improvements to RANS models applied to separated flows
Ablating Woven Thermal Protection System Materials Under High Shear Flow Conditions
Ongoing Aeroelastic Optimization Research at NASA LaRC, Aeroelasticity Branch
Nonlinear Development and Secondary Instability of Traveling Crossflow Vortices
Inside NASA’s X-57 Configuration - More than Just Electrifying an Airplane
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
Application of the CATNLF Design Method to a Transonic Transport Empennage Using CDISC
Magnetic Suspension Wind Tunnel Reconstruction Using an Extended Kalman Filter Framework
Method for Extracting Aerodynamic Coefficients and Winds On-the-Fly Using Real-Time GPS Data
High-Order Methods in NASA's Next Generation of Computational Fluid Dynamics Tools
Recent Aero Modeling Recommendations for Upset Training Simulations: The ICATEE Perspective
Asymmetric Flow State Switching on the Space Launch System (SLS) Block 2 Crew Vehicle
Comparison of Aerodynamic Analysis Tools Applied to a Propeller-Blown Wing
Kestrel Results for DPW-VII Including Adaptive Mesh and IDDES Computations
Magnetic Suspension Wind Tunnel Reconstruction Using an Extended Kalman Filter Framework
Aeroelastic Analysis of Highly Flexible Wings with Linearized Frequency-Domain Aerodynamics
Preparations for Tomographic Background-Oriented Schlieren at the 31-Inch Mach 10 Wind Tunnel
Unsteady Surface Pressures on the Space Launch System Block 1B Cargo Liftoff Configuration
One Giant Leap for Womankind: An Aerodynamic Study of the SLS Rocket ft. Pressure-Sensitive Paint
Design and Fabrication of the Boundary Layer Ingesting Tailcone System CRM-TCT Model in the NTF
Development of Aerodynamic Loads Databases for the Space Launch System Booster Separation Event
AeroFusion: Data Fusion and Uncertainty Quantification for Entry Vehicles
Direct Numerical Simulation of A Turbulent Separation Bubble With Sweep
Ongoing Subsonic Aeroelastic Optimization Research at NASA LaRC, Aeroelasticity Branch