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.
Keywords
aeroplane stall; aerodynamics principles; wing mechanism; DCS World
Full Text:
PDFDOI: https://doi.org/10.35116/aa.2023.0012
Refbacks
- There are currently no refbacks.
Copyright (c) 2023 Jozef Sabo, Branko Mikula, Peter Kaľavský, Jaroslav Gahura
This work is licensed under a Creative Commons Attribution 4.0 International License.