科技报告详细信息
A Summary of the NASA Design Environment for Novel Vertical Lift Vehicles (DELIVER) Project
Theodore, Colin R
关键词: TILT WING AIRCRAFT;    AIRCRAFT DESIGN;    VERTICAL LANDING;    VERTICAL TAKEOFF;    ROTARY WINGS;    COMPUTATIONAL FLUID DYNAMICS;    HYBRID PROPULSION;    ELECTRIC PROPULSION;    AUTONOMY;    AEROACOUSTICS;    PILOTLESS AIRCRAFT;    LIFT DRAG RATIO;    WIND TUNNEL TESTS;    FLIGHT SIMULATION;    PRESSURE DISTRIBUTION;   
RP-ID  :  ARC-E-DAA-TN51290
美国|英语
来源: NASA Technical Reports Server
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【 摘 要 】
The number of new markets and use cases being developed for vertical take-off and landing vehicles continues to explode, including the highly publicized urban air taxi and package deliver applications. There is an equally exploding variety of novel vehicle configurations and sizes that are being proposed to fill these new market applications. The challenge for vehicle designers is that there is currently no easy and consistent way to go from a compelling mission or use case to a vehicle that is best configured and sized for the particular mission. This is because the availability of accurate and validated conceptual design tools for these novel types and sizes of vehicles have not kept pace with the new markets and vehicles themselves. The Design Environment for Novel Vertical Lift Vehicles (DELIVER) project was formulated to address this vehicle design challenge by demonstrating the use of current conceptual design tools, that have been used for decades to design and size conventional rotorcraft, applied to these novel vehicle types, configurations and sizes. In addition to demonstrating the applicability of current design and sizing tools to novel vehicle configurations and sizes, DELIVER also demonstrated the addition of key transformational technologies of noise, autonomy, and hybrid-electric and all-electric propulsion into the vehicle conceptual design process. Noise is key for community acceptance, autonomy and the need to operate autonomously are key for efficient, reliable and safe operations, and electrification of the propulsion system is a key enabler for these new vehicle types and sizes. This paper provides a summary of the DELIVER project and shows the applicability of current conceptual design and sizing tools novel vehicle configurations and sizes that are being proposed for urban air taxi and package delivery type applications.
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