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- W2805736802 abstract "Unmanned Aerial System (UAS) design and development has been focused largely on aerial surveillance and photography or high payload applications. As yet there has not been a large effort expended in developing high speed UAS technology on a small enough scale suitable for commercial use. Despite this there are applications such as emergency medical response that would benefit from the development of this concept. This project aims to produce a working propulsion system capable of both high speed ght and vertical take-o and landing for a UAS under 10kg. In the course of the project a JetCAT P80SE Micro Gas turbine is procured and characterised using an instrumentation set designed, calibrated, and implemented in house as part of this project. The exhaust properties of the engine are then used in a series of iterative Computational Fluid Dynamic and Finite Element Analysis studies to produce a thrust vectoring nozzle capable of withstanding the thermal and pressure loads. This nozzle uses a bespoke design to vector thrust through a full 90 degree bend with a very low thrust loss. The results indicate that although there is room for improvement the design will meet its performance requirements and thus be able to progress to be integrated into a ying platform." @default.
- W2805736802 created "2018-06-13" @default.
- W2805736802 creator A5037051061 @default.
- W2805736802 date "2017-10-27" @default.
- W2805736802 modified "2023-09-26" @default.
- W2805736802 title "Design of a Thrust Vectoring Nozzle for a Micro Gas Turbine" @default.
- W2805736802 hasPublicationYear "2017" @default.
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