Aerodynamic technologies to improve aircraft performance
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
Estimation of Vehicle-Level Fuel Burn Benefits of Aircraft Formation Flight
Minimum-Drag Fault-Tolerant Aircraft Control Allocation via Online Lifting Line Calculation
Retrospective on the Common Research Model for Computational Fluid Dynamics Validation Studies
Waverider Design Using Osculating Method
Analysis of a Wing–Fuselage Biplane with Trailing-Edge Flaps in Low-Speed Flow
Maximum Range for Battery-Powered Aircraft
Preliminary Design of a Solar-Powered Hybrid Airship
Spectral Proper Orthogonal Decomposition Reduced-Order Model for Analysis of Aerothermoelasticity
Performance Assessment of a Transonic Wing–Body Configuration with Riblets Installed
Modern Implementation and Evaluation of Lifting-Line Theory for Complex Geometries
Correction: Optimal Hyperelliptic Cambered Span Configurations for Minimum Drag
Aerodynamic Optimization Trade Study of a Box-Wing Aircraft Configuration
Analysis of Low-Speed Stall Aerodynamics of a Business Jets Wing Using STAR-CCM+
MSFC Advanced Concepts Office and the Iterative Launch Vehicle Concept Method
Low-Boom/Low-Drag Design Optimization of Innovative Supersonic Transport Configuration