Effects of Propeller Position and Rotation Direction on the Ishii Wing at a Low Reynolds Number

Author:

FUJITA Koji1,KURANE Kakeru2,TAKAHASHI Koichi1,NAGAI Hiroki1

Affiliation:

1. Institute of Fluid Science, Tohoku University

2. Department of Aerospace Engineering, Graduate School of Engineering, Tohoku University

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Reference20 articles.

1. 1) Oyama, A.: Conceptual Design of Mars Airplane for MELOS1, JSASS-2010-4469, 2010 (in Japanese).

2. 2) Fujita, K., Nagai, H., and Asai, K.: Conceptual Design of a Miniature, Propeller-Driven Airplane for Mars, Proc. of 50th AIAA Aerospace Sciences Meeting, Nashville, Tennessee, AIAA-2012-0847, 2012.

3. 3) Nagai, H., Oyama, A., and Mars Airplane Working Group: Mission Scenario of Mars Exploration by Airplane, Proc. of the 2013 Asia-Pacific International Symposium on Aerospace Technology, Takamatsu, Japan, 2013, pp. 1–6.

4. 4) Nagai, H., Oyama, A., and Mars Airplane Working Group: Development of Mars Exploration Aerial Vehicle in Japan, Proc. of the 30th International Symposium on Space Technology and Science, Kobe, Japan, 2015-k-46, 2015.

5. 5) Nagai, H. and Mars Airplane Working Group: Aerodynamic Challenge to Realize Mars Airplane, Proc. of the 30th International Symposium on Space Technology and Science, Kobe, Japan, 2015-k-47, 2015.

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