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- W2335449670 abstract "The interaction of the wall jet formed when a jet exhaust impinges on the ground and the free stream flow creates a ground vortex which can have a significant effect on the aerodynamic characteristics as a STOL airplane configuration nears the ground. significant variation in the lift and pitching moment coefficients can be encountered. These variations have been seen during test of STOL jet lift configurations and have been encountered with the deployment of thrust reversers near the ground. The ground vortex and the effect of various ground simulations have been investigated and the results reported in prevlous papers. This paper discusses the effect of the ground vortex on the lift and pitching moment of a generic STOL configuration." @default.
- W2335449670 created "2016-06-24" @default.
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- W2335449670 date "1993-08-22" @default.
- W2335449670 modified "2023-09-25" @default.
- W2335449670 title "A correlation of the effects of the ground vortex on the aerodynamic characteristics of a generic STOL aircraft configuration" @default.
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- W2335449670 doi "https://doi.org/10.2514/6.1993-4864" @default.
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