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Aircraft
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Conceptual design of PrandtlPlane civil transport aircraft
Leading-Edge Cone Method for Waverider Design
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
Next Generation Transport Concepts and Enabling Technology Research at NASA
Progress Towards Understanding Fan Inlet Implications of Top-Mounted Propulsion
Waverider Design Using Osculating Method
Optimization of an Air Core Dual Halbach Array Axial Flux Rim Drive for Electric Aircraft
Turboelectric Aircraft Drive Key Performance Parameters and Functional Requirements
Modeling Turboshaft Engines for the Revolutionary Vertical Lift Technology Project
Propulsion Technologies for Future Aircraft Generations: A NASA Perspective
High Crosswind-Tolerance Airplane by Adjusting Dihedral Angle and Vertical Tail Volume
Systematic Methodology for Aircraft Concept Development with Application to Transitional Aircraft
Parameterization of Curvilinear Spars and Ribs for Optimum Wing Structural Design
Overview of NASA Electrified Aircraft Propulsion Research for Large Subsonic Transports
Overview of NASA Electrified Aircraft Propulsion Research for Large Subsonic Transports
Overview of NASA Electrified Aircraft Propulsion Research for Large Subsonic Transports
Overview of NASA Electrified Aircraft Propulsion Research for Large Subsonic Transports