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- W2021988552 abstract "Low speed wind tunnel tests were conducted to assess four methods for attaining thrust modulation for V/STOL aircraft. The four methods were: (1) fan speed change, (2) fan nozzle exit area change, (3) variable pitch rotor (VPR) fan, and (4) variable inlet guide vanes (VIGV). The interrelationships between inlet and thrust modulation system were also investigated using a double slotted inlet and thick lip inlet. Results can be summarized as: (1) the VPR and VIGV systems were the most promising, (2) changes in blade angle to obtain changes in fan thrust have significant implications for the inlet, and (3) both systems attained required level of thrust with acceptable levels of fan blade stress." @default.
- W2021988552 created "2016-06-24" @default.
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- W2021988552 date "1981-08-17" @default.
- W2021988552 modified "2023-09-23" @default.
- W2021988552 title "Thrust modulation methods for a subsonic V/STOL aircraft" @default.
- W2021988552 doi "https://doi.org/10.2514/6.1981-2633" @default.
- W2021988552 hasPublicationYear "1981" @default.
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