Masahiro Kono
Masahiro Kono has a total of 6 co-authors. Here are the top co-authors by number of shared publications:
Akiyoshi Masaki
早稲田大学基幹理工学研究科機械科学・航空宇宙専
1 shared publicationDaisaku Masaki
宇宙航空研究開発機構航空技術部
1 shared publication- Junichi Kazawa
Japan Aerospace Exploration Agency, 7-44-1 Jindaiji-Higashimachi, Chofu-shi, Tokyo 182-8522, Japan
1 shared publication - Keiichi Okai
Japan Aerospace Exploration Agency, Chofu, Japan
1 shared publication - Tetsuya Sato
Waseda University
1 shared publication Tomoya Kogirima
早稲田大学基幹理工学部機械科学・航空宇宙学
1 shared publication
Latest Publications
- 1 January 2023
- Published by Japan Society for Aeronautical and Space Sciences in Aerospace Technology Japan, the Japan Society for Aeronautical and Space Sciences
- Vol. 22, 11-19
Experimental and Analytical Evaluation on the Effects of the Boundary Layer Ingestion (BLI) Using a Simple Engine/Airframe Integration Model
The benefit of Boundary Layer Ingestion (BLI) was evaluated by wind tunnel test and analysis. Using a simple engine/airframe model which is composed of an airfoil based on NACA0012, an electric fan and an electric motor, wind tunnel test was conducted. Net streamwise force and electric power were mainly measured. Based on the power balance method originally described by Drela, the concept of conversion efficiency was added to separate demerit of BLI. By using conversion efficiency, mechanical power was changed to electrical power and making it easy to understand benefit of BLI. This analytical method was fit with experimental data and well represent BLI benefit. At cruise condition in 40m/s, BLI configuration needs lower 7.66% electrical power than nonBLI configuration.
- 1 January 2023
- Published by Japan Society for Aeronautical and Space Sciences in Aerospace Technology Japan, the Japan Society for Aeronautical and Space Sciences
- Vol. 22, 11-19
Experimental and Analytical Evaluation on the Effects of the Boundary Layer Ingestion (BLI) Using a Simple Engine/Airframe Integration Model
The benefit of Boundary Layer Ingestion (BLI) was evaluated by wind tunnel test and analysis. Using a simple engine/airframe model which is composed of an airfoil based on NACA0012, an electric fan and an electric motor, wind tunnel test was conducted. Net streamwise force and electric power were mainly measured. Based on the power balance method originally described by Drela, the concept of conversion efficiency was added to separate demerit of BLI. By using conversion efficiency, mechanical power was changed to electrical power and making it easy to understand benefit of BLI. This analytical method was fit with experimental data and well represent BLI benefit. At cruise condition in 40m/s, BLI configuration needs lower 7.66% electrical power than nonBLI configuration.