Current capabilities and challenges of NDARC and SUAVE for eVTOL aircraft design and analysis

Keyphrases

• Current Capability 100%
• Rotor 100%
• Wingspan 100%
• Aircraft Design 100%
• EVTOL 100%
• SUAVE 100%
• Takeoff Weight 100%
• Sweeping 50%
• Initial Design 50%
• Further Development 50%
• Area of Uncertainty 50%
• Design Modeling 50%
• Design Assumptions 50%
• Publicly Available Information 50%
• Aerodynamic Performance 50%
• CorA 50%
• Trade Studies 50%
• Reference Mission 50%
• Conceptual Methods 50%

Engineering

• Wingspan 100%
• Rotor Radius 100%
• Takeoff Weight 100%
• Starting Point 50%
• Initial Design 50%
• Aerodynamic Performance 50%
• Trade Study 50%