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Scaling Analysis of Propeller-Driven Aircraft for Mars Exploration

机译：用于火星探测的螺旋桨驱动飞机的比例分析

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摘要

The scaling relations between the performance parameters of propeller-driven aircraft flying on Mars and Earth are discussed, including the cruising velocity, power required for cruising flight, and propulsive power generated by propellers. The power ratio criterion for feasible cruising flight of propeller-driven aircraft on Mars is proposed, and the relevant design parameters are identified. This criterion is first used to examine the feasibility of typical and nontypical aircraft for cruising flight on Mars, and then applied as a guideline to the preliminary design of the sample Martian aircraft. In addition, the constraints on the rotational speed of a propeller in cruising flight on Mars are given, which should be considered in the design of propellers. The methods developed in this paper are also applicable to other space exploration aircraft for Venus and Titan.
机译：讨论了在火星和地球上飞行的螺旋桨驱动飞机的性能参数之间的比例关系，包括巡航速度，巡航飞行所需的功率以及螺旋桨产生的推进力。提出了螺旋桨驱动飞机在火星上可行巡航飞行的功率比准则，并确定了相关的设计参数。该标准首先用于检查典型和非典型飞机在火星上巡航飞行的可行性，然后将其用作样本火星飞机初步设计的指南。另外，给出了在火星上巡航飞行中螺旋桨转速的限制条件，在螺旋桨的设计中应予以考虑。本文开发的方法也适用于金星和土卫六的其他太空探索飞机。

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  • 来源
    《Journal of Aircraft》 |2013年第5期|1593-1604|共12页
  • 作者

    Tianshu Liu; Akira Oyama; Kozo Fujii;

  • 作者单位

    Professor, Department of Mechanical and Aeronautical Engineering. Western Michigan University, Kalamazoo, Michigan 49008;

    Associate Professor, Department of Space Flight Systems. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Sagamihara 252-5210, Japan;

    Professor, Department of Space Flight Systems. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Sagamihara 252-5210, Japan;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
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