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Aerodynamic design of transonic UAV glider

By Marián Kóňa

Abstract

This master thesis is focused on aerodynamic design of transonic glider, which is assigned for following an airliner at cruising regime of flight. Main goal of the thesis is to determine basic geometrical design of airplane with respect to Whitcomb aera rule, mass analysis and drag polar. Weight analysis includes determining center of gravity according to longitudinal static stability margin. The drag polar of the airplane is determine for cruising regime of flight, that means the regime of following an airliner

Topics: Whitcombovo pravidlo ploch; Transonic; polára; hmotnostní rozbor; Transsonika; center of gravity position; podélná statická stabilita; kluzák; Whitcomb area rule; drag polar; mass analysis; centráž; glider; longitudinal static stability
Publisher: Vysoké učení technické v Brně. Fakulta strojního inženýrství
Year: 2015
OAI identifier: oai:invenio.nusl.cz:232008
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