Multidisciplinary Aircraft Design and Technology Assessment (Z)

该项目研究了超高压反应器推进和前掠翼的配置，旨在确定飞行中BLC压气机用于巡航飞行层流翼流的潜力。为了在起飞时进一步减轻发动机的负担，为压气机提供独立的电源保证了一些优势，这些优势将在飞机整体水平上进行详细调查和最终评估。在飞机设计的背景下，噪声评估将集中在螺旋桨和Coanda襟翼的增强源模型上。此外，建议的SFB降噪技术将会实施。该项目的目的还在于与现有的SFB参考车辆相比，研究非常规配置的技术和声学潜力。

This project investigates configurations with UHBR propulsion and a forward swept wing, and aims to identi-fy the potential of in-flight BLC compressors for cruise-flight laminar wing flow. To further relieve the en-gines at takeoff, an independent power supply for the compressors promises advantages that will be inves-tigated in detail and conclusively evaluated on the overall aircraft level. Noise assessment in the context of the aircraft design will focus on enhanced source models for the propeller and for the Coanda flap. Fur-thermore, proposed SFB noise reduction technologies will be implemented. The objective of this project is also to examine the technical as well as the acoustic potential of unconventional configurations compared to the current SFB reference vehicles.