AEROPLANE STALLS AND LOSS OF ALTITUDE

Peter Kaľavský, Jozef Sabo, Branko Mikula, Jaroslav Gahura

Abstract


The aim of this study is an experimental verification of   loss of altitude during a stall which is  performed on a specific aeroplane type in a flight simulator environment. Also, the paper deals with a methodology how to control   an aeroplane entering stall conditions and its recovery  in the flight simulator. An experimental verification of altitude loss during the stall is a part of this paper too. Values collected  from various  measurements of  loss of altitude during stalls were recorded into specific tables. Recorded values were diversified according specific stall types.

Keywords


aeroplane stall; aerodynamics principles; wing mechanism; DCS World

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DOI: https://doi.org/10.35116/aa.2023.0012

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Copyright (c) 2023 Jozef Sabo, Branko Mikula, Peter Kaľavský, Jaroslav Gahura

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