Next Generation Transport Concepts and Enabling Technology Research at NASA
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
Missile Aerodynamics for Ascent and Re-entry
Exploration of Configuration Options for a Large Civil Compound Helicopter
Method for Estimating the Sonic-Boom Characteristics of Lifting Canard-Wing Aircraft Concepts
Wind Tunnel Tests of Several Ducted Propellers in Non-Axial Flow
Overview of NASA Electrified Aircraft Propulsion Research for Large Subsonic Transports
Auralization of Hybrid Wing Body Aircraft Flyover Noise from System Noise Predictions
Wind Tunnel Feasibility Study of Aerodynamic Reefing of Subsonic Parachutes
Re-Entry Vehicle of Similar Article
Progress Towards Understanding Fan Inlet Implications of Top-Mounted Propulsion
Aeroelastic Optimization of Generalized Tube and Wing Aircraft Concepts Using HCDstruct Version 2.0
Theory/Test Correlation of Helicopter Rotor Blade Element Airloads in the Blade Stall Regime
CFD Predictions for Transonic Performance of the ERA Hybrid Wing-Body Configuration