Aerodynamic Performance of an Aircraft with Aft-Fuselage Boundary-Layer-Ingestion Propulsion
Exergy-Based Performance Assessment of the NASA Common Research Model
Conceptual Sizing of Vertical Lift Package Delivery Platforms
Full-Aircraft Energy-Based Force Decomposition Applied to Boundary-Layer Ingestion
Development of Deformed Computer-Aided Design Geometries for the Sixth Drag Prediction Workshop
Deep Learning Based Reduced Order Model for Airfoil-Gust and Aeroelastic Interaction
Noncertainty-Equivalent Adaptive Wing-Rock Control via Chebyshev Neural Network
Convex Approach to Three-Dimensional Launch Vehicle Ascent Trajectory Optimization
Computational Fluid Dynamics Modeling of Helicopter Fuselage Drag
Unsteady Aerostructure Coupled Adjoint Method for Flutter Suppression
Dynamic Distributed Morphing Control of an Aeroelastic Wing for a Small Drone
Slowed Hingeless Rotor Wind Tunnel Tests and Validation at High Advance Ratios
Application of Automatic Differentiation for Tilt-Rotor Aircraft Flight Dynamics Analysis
Refined Tetrahedral Meshes with Mach Cone Aligned Prisms for Sonic Boom Analysis
Trim Analyses of Mass-Actuated Airplane in Cruise and Steady-State Turn
Multidisciplinary Design Optimization of Low-Boom Supersonic Aircraft with Mission Constraints
Dynamic Simulation and Control of Mass-Actuated Airplane
Systematic Methodology for Aircraft Concept Development with Application to Transitional Aircraft
Analysis of a Wing–Fuselage Biplane with Trailing-Edge Flaps in Low-Speed Flow