Compressibility Effects on Aerodynamic Characteristics and Flow Fields of Mars Helicopter Rotor-Reference-Cited by-同舟云学术

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Compressibility Effects on Aerodynamic Characteristics and Flow Fields of Mars Helicopter Rotor

Published:2023-06-08 Issue: Volume: Page:
ISSN:
Container-title:AIAA AVIATION 2023 Forum
language:
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Author:

Yoshikawa Kota¹,Buto Yuta¹,Sato Makoto¹,Oyama Akira²,Sugiura Masahiko³,Tanabe Yasutada³,Kimura Keita³,Takekawa Kuniyuki⁴,Kishi Yuki⁵,Kanazaki Masahiro⁵

Affiliation:

1. Kogakuin Daigaku

2. Uchu Koku Kenkyu Kaihatsu Kiko Uchu Kagaku Kenkyujo

3. Uchu Koku Kenkyu Kaihatsu Kiko

4. Ryoyu Systems Company, Ltd.

5. Tokyo Toritsu Daigaku

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2023-4000

Reference24 articles.

1. Aeromechanical Analysis of a Next-Generation Mars Hexacopter Rotor

2. Atypical pit craters on Mars: New insights from THEMIS, CTX, and HiRISE observations

3. Conceptual Helicopter Design for Exploration of Pit craters and Caves on Mars

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