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- W3132140818 abstract "Despite the rapid evolution of technology in both the mechanical and aviation fields, one area thatremains unexplored is the ground effect (GE) and its potential implication on land, sea and air vehicles of thefuture. In this regard, the development and implementation of Wing-in-Ground (WIG) crafts have particularlybeen lagging behind. WIG crafts are essentially vessels which are operated within the GE, whereby, an improvedlift-to-drag (L/D) ratio is considered as a major enabling factor for aerodynamics improvement. Because of theunique properties within the GE, WIG crafts are inherently energy-efficient and performance-oriented vessels.Their versatility also makes them ideal for a wide range of applications encompassing both military and civilianuse. The flying airboat (FA) concept is an example of a WIG craft that utilizes these characteristics, with a designthat seeks to add the benefit of vertical take-off and landing (VTOL). In this study, the approach adopted fordesigning a mathematical control model of the concept is explored. The analysis findings indicate that thecontrollability of a WIG craft, such as the FA, is mostly reliant upon the fundamental equations of motion.Incorporation of span dominated GE (SDGE) into the control model substantially improves the lift-to-drag ratioand therefore, the overall performance of the WIG. The investigation concludes that implementing amanoeuvrability control model for the FA is viable with minor changes to the presented physical design." @default.
- W3132140818 created "2021-03-01" @default.
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- W3132140818 date "2021-02-16" @default.
- W3132140818 modified "2023-09-27" @default.
- W3132140818 title "Preliminary Investigation into the design of a Mathematical Control Model for Flying Airboat Concept within Ground Effect" @default.
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