AEROPLANE STALLS AND LOSS OF ALTITUDE

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.