Correction to: Understanding the fixed pitch RPM-controlled rotor modeling for the conceptual design of UAM vehicles

Q2 Engineering

CEAS Aeronautical Journal Pub Date : 2024-01-31 DOI:10.1007/s13272-024-00713-1

K. Atci, P. Weiand, Feyyaz Guner

引用次数: 0

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更正：了解用于 UAM 飞行器概念设计的固定螺距转速控制转子模型

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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来源期刊

CEAS Aeronautical Journal Engineering-Aerospace Engineering

CiteScore

3.40

自引率

0.00%

发文量

期刊介绍： The CEAS Aeronautical Journal has been created under the umbrella of CEAS to provide an appropriate platform for excellent scientific publications submitted by scientists and engineers. The German Aerospace Center (DLR) and the European Space Agency (ESA) support the Journal.The Journal is devoted to publishing results and findings in all areas of aeronautics-related science and technology as well as reports on new developments in design and manufacturing of aircraft, rotorcraft, and unmanned aerial vehicles. Of interest are also (invited) in-depth reviews of the status of development in specific areas of relevance to aeronautics, and descriptions of the potential way forward. Typical disciplines of interest include flight physics and aerodynamics, aeroelasticity and structural mechanics, aeroacoustics, structures and materials, flight mechanics and flight control, systems, flight guidance, air traffic management, communication, navigation and surveillance, aircraft and aircraft design, rotorcraft and propulsion.The Journal publishes peer-reviewed original articles, (invited) reviews and short communications.