Masayuki Anyoji

Associate Professor

National University Corporation Kyushu University, Thermo Fluid Dynamics Division

Websitehttps://hyoka.ofc.kyushu-u.ac.jp/search/details/K005622/index.html

Source: Scopus
Calculated based on no. of publications stored in Pure and citations from Scopus

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222 Citations
10 h-Index
15 Conference contribution
10 Article
1 Paper

Investigation of Mach number effects on flow over a flat plate at Reynolds number of 1.0 × 10⁴by schlieren visualization
Kusama, K., Nagata, T., Anyoji, M., Nonomura, T., Asai, K. & Nagata, T., Feb 2021, In: Fluid Dynamics Research. 53, 1, 015513.
Research output: Contribution to journal › Article › peer-review
1 Citation (Scopus)
Aerodynamics of owl-like wing model at low reynolds numbers
Aono, H., Kondo, K., Nonomura, T., Anyoji, M., Oyama, A., Fujii, K. & Yamamoto, M., 2020, In: Transactions of the Japan Society for Aeronautical and Space Sciences. 63, 1, p. 8-17 10 p.
Research output: Contribution to journal › Article › peer-review

Open Access
1 Citation (Scopus)
Experimental and rans analysis of full mars airplane configurations
Taniguchi, S., Oyama, A., Okamoto, M., Anyoji, M., Fujita, K. & Nagai, H., 2020, AIAA Scitech 2020 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, p. 1-14 14 p. (AIAA Scitech 2020 Forum; vol. 1 PartF).
Research output: Chapter in Book/Report/Conference proceeding › Conference contribution
A study on development of airfoil shape toward low reynolds-number dependence of aerodynamic characteristics under low-reynolds-number-flow conditions
Aono, H., Anyoji, M., Hamada, D., Wakui, S. & Tatsukawa, T., 2018, AIAA Aerospace Sciences Meeting. 210059 ed. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aerospace Sciences Meeting, 2018; no. 210059).
Research output: Chapter in Book/Report/Conference proceeding › Conference contribution
2 Citations (Scopus)
Identification of acoustic wave propagation pattern of a supersonic jet using frequency-domain POd
Ozawa, Y., Nonomura, T., Anyoji, M., Mamori, H., Fukushima, N., Oyama, A., Fujii, K. & Yamamoto, M., 2018, In: Transactions of the Japan Society for Aeronautical and Space Sciences. 61, 6, p. 281-284 4 p.
Research output: Contribution to journal › Article › peer-review

2 Citations (Scopus)

Investigation of Mach number effects on flow over a flat plate at Reynolds number of 1.0 × 104by schlieren visualization

Aerodynamics of owl-like wing model at low reynolds numbers

Experimental and rans analysis of full mars airplane configurations

A study on development of airfoil shape toward low reynolds-number dependence of aerodynamic characteristics under low-reynolds-number-flow conditions

Identification of acoustic wave propagation pattern of a supersonic jet using frequency-domain POd

Investigation of Mach number effects on flow over a flat plate at Reynolds number of 1.0 × 10⁴by schlieren visualization