Aerodynamic technologies to improve aircraft performance
Estimation of Vehicle-Level Fuel Burn Benefits of Aircraft Formation Flight
Leading-Edge Cone Method for Waverider Design
Control Authority of a Camber Morphing Flying Wing
Next Generation Transport Concepts and Enabling Technology Research at NASA
Waverider Design Using Osculating Method
Retrospective on the Common Research Model for Computational Fluid Dynamics Validation Studies
Minimum-Drag Fault-Tolerant Aircraft Control Allocation via Online Lifting Line Calculation
Analysis of a Wing–Fuselage Biplane with Trailing-Edge Flaps in Low-Speed Flow
Preliminary Design of a Solar-Powered Hybrid Airship
Analysis of Low-Speed Stall Aerodynamics of a Business Jets Wing Using STAR-CCM+
Spectral Proper Orthogonal Decomposition Reduced-Order Model for Analysis of Aerothermoelasticity
Low-Boom/Low-Drag Design Optimization of Innovative Supersonic Transport Configuration
Maximum Range for Battery-Powered Aircraft
MSFC Advanced Concepts Office and the Iterative Launch Vehicle Concept Method
Modern Implementation and Evaluation of Lifting-Line Theory for Complex Geometries
Performance Assessment of a Transonic Wing–Body Configuration with Riblets Installed
Aerodynamic Optimization Trade Study of a Box-Wing Aircraft Configuration
Correction: Optimal Hyperelliptic Cambered Span Configurations for Minimum Drag
Aerodynamic Design Optimization Studies of a Blended-Wing-Body Aircraft
Missile Aerodynamics for Ascent and Re-entry
Computational Prediction of Annular Wing Aerodynamic Characteristics
Drag Minimization Based on the Navier–Stokes Equations Using a Newton–Krylov Approach
Vortex Interaction Characteristics of Multiswept Wings at Subsonic Speeds
Exploration of Configuration Options for a Large Civil Compound Helicopter
Experimental Investigation of the Coupling Process of Laminar Wings at Their Tips
Buffet-Onset Constraint Formulation for Aerodynamic Shape Optimization
Method for Estimating the Sonic-Boom Characteristics of Lifting Canard-Wing Aircraft Concepts
Aeroelastic Scaling of a High-Aspect-Ratio Wing Incorporating a Semi-Aeroelastic Hinge
Computational Assessment of Transonic Airfoil-Gust Aeroelastic Response
Wind Tunnel Tests of Several Ducted Propellers in Non-Axial Flow
Folding Wingtips for Improved Roll Performance
Efficient Surrogate Modelling of Nonlinear Aerodynamics in Aerostructural Coupling Schemes
Analysis of the Aerodynamic Benefit from Boundary Layer Ingestion for Transport Aircraft
Numerical Study of Aerodynamic Performance of a Multirotor Unmanned-Aerial-Vehicle Configuration
Two Aerodynamic Mid-Fidelity Approaches on a Distributed Propulsion Wing
Aerodynamic Design Optimization of a Transonic Strut-Braced-Wing Regional Aircraft
Unsteady Aeroelastic Analysis of the Semi Aeroelastic Hinge Including Local Geometric Nonlinearities
Investigation of a Morphing Wing Solar-Powered Unmanned Aircraft with Enlarged Flight Latitude
Aerodynamic Shape Optimization of Common Research Model Wing–Body–Tail Configuration
Unsteady Aerostructure Coupled Adjoint Method for Flutter Suppression
Multidisciplinary Design Optimization of Low-Boom Supersonic Aircraft with Mission Constraints