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- W2012076203 abstract "An investigation has been conducted in the Langley V/STOL tunnel to determine the low speed aerodynamic characteristics of a close-coupled canard-wing configuration using spanwise blowing and a vectored-engine-over-wing powered lift concept. The effects of spanwise blowing in conjunction with thrust vectoring are discussed. These effects were studied at M = 0.19 for a range of model angle of attack and engine nozzle pressure ratio. The results indicate combined use of spanwise blowing and thrust vectoring can provide significant performance improvements throughout the angle-of-attack range tested." @default.
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- W2012076203 date "1978-07-25" @default.
- W2012076203 modified "2023-09-27" @default.
- W2012076203 title "Low speed aerodynamic characteristics of a vectored-engine-over-wingconfiguration" @default.
- W2012076203 cites W2328210143 @default.
- W2012076203 doi "https://doi.org/10.2514/6.1978-1081" @default.
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