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Aircraft
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Leading-Edge Cone Method for Waverider Design
Conceptual design of PrandtlPlane civil transport aircraft
Estimation of Vehicle-Level Fuel Burn Benefits of Aircraft Formation Flight
Comparative Assessment of Aircraft System Noise Simulation Tools
Exploration of Configuration Options for a Large Civil Compound Helicopter
Modeling Turboshaft Engines for the Revolutionary Vertical Lift Technology Project
Next Generation Transport Concepts and Enabling Technology Research at NASA
Progress Towards Understanding Fan Inlet Implications of Top-Mounted Propulsion
Propulsion Technologies for Future Aircraft Generations: A NASA Perspective
Waverider Design Using Osculating Method
Optimization of an Air Core Dual Halbach Array Axial Flux Rim Drive for Electric Aircraft
X-48B Preliminary Flight Test Results
High Crosswind-Tolerance Airplane by Adjusting Dihedral Angle and Vertical Tail Volume
Turboelectric Aircraft Drive Key Performance Parameters and Functional Requirements
Parameterization of Curvilinear Spars and Ribs for Optimum Wing Structural Design