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