Fluidic thrust vectoring (FTV), an ability of air vehicles to manipulate the nozzle flow deflect their longitudinal axis, can satisfy the modern aircraft requirements dramatically. Numerical and experimental studies of FTV are performed with a nozzle pressure ratio (NPR) of 4–10, a secondary pressure ratio (SPR) of 1, 2 or 3, and two different secondary jet locations. Numerical simulations of the nozzle flow are done with solving the Navier-Stokes equations, and the input parameters are set to match the experimental conditions. The thrust pitching moment and the thrust pitching angle are determined to evaluate the FTV performance.
雑誌名
室蘭工業大学紀要
巻
62
ページ
3 - 6
発行年
2013-03-18
注記
特集 : Special Section for the Papers Presented at the Symposium on Mechanical Engineering, Industrial Engineering, and Robotics held at Noboribetsu, Hokkaido, Japan on 11 - 12 January 2012
Numerical and Experimental Investigations of Fluidic Thrust Vectoring
kiyo62_pp3-6.pdf
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