A copy of this work was available on the public web and has been preserved in the Wayback Machine. The capture dates from 2022; you can also visit the original URL.
The file type is application/pdf
.
Research Activity on Aerodynamics for High-Lift Configuration of Civil Transport Aircraft at JAXA
航空機研究の最前線 JAXAにおける旅客機高揚力形態の空力技術の研究
2007
Journal of Japan Society of Fluid Mechanics
航空機研究の最前線 JAXAにおける旅客機高揚力形態の空力技術の研究
In the aerodynamic design of high-lift configuration of civil transport aircraft at takeoff and landing, there are strong demands for improvement in the capability of Computational Fluid Dynamics (CFD), since its geometry and flow physics are very complicated to be well predicted by CFD. This article briefly presents the research activity at JAXA aiming at the improvement of CFD for high-lift configuration using an experimental model equipped with high-lift devices, fuselage, nacelle-pylon, slat tracks and Flap Track Fairings (FTF).
doi:10.11426/nagare1982.26.251
fatcat:tmieaocxjvcelpxyh2kljavf5q