TY - GEN
T1 - Experimental and numerical evaluation of boundary layer ingestion effect with engine/airframe integration model
AU - Okai, Keiichi
AU - Mitani, Yoshihiro
AU - Yoshida, Hidekazu
AU - Ogushi, Shotaro
AU - Tsuruta, Ryosuke
AU - Okuno, Akiko
AU - Sato, Tetsuya
AU - Harada, Masashi
N1 - Funding Information:
The authors acknowledge the guidance and support of Dr. T. Hirotani of JAXA during the wind tunnel test.
PY - 2019
Y1 - 2019
N2 - Boundary layer ingestion benefit is experimentally and numerically investigated. Simple 2-dimensional-airfoil shape airframe with electric fan configures an airframe/engine integration. Wind tunnel test was conducted with force measurement. Accompanying CFD calculation was conducted with a solver FaSTAR developed by JAXA. Experimental result shows that both of the 2 BLI configurations give larger forward thrust than referential nonBLI configuration with same power consumption. The difference between the 2 BLI case results was investigated. CFD result shows quantitative agreement with the experimental result, though performance metrics is different.
AB - Boundary layer ingestion benefit is experimentally and numerically investigated. Simple 2-dimensional-airfoil shape airframe with electric fan configures an airframe/engine integration. Wind tunnel test was conducted with force measurement. Accompanying CFD calculation was conducted with a solver FaSTAR developed by JAXA. Experimental result shows that both of the 2 BLI configurations give larger forward thrust than referential nonBLI configuration with same power consumption. The difference between the 2 BLI case results was investigated. CFD result shows quantitative agreement with the experimental result, though performance metrics is different.
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U2 - 10.2514/6.2019-3852
DO - 10.2514/6.2019-3852
M3 - Conference contribution
AN - SCOPUS:85095968914
SN - 9781624105906
T3 - AIAA Propulsion and Energy Forum and Exposition, 2019
BT - AIAA Propulsion and Energy Forum and Exposition, 2019
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Propulsion and Energy Forum and Exposition, 2019
Y2 - 19 August 2019 through 22 August 2019
ER -