Author:
Malik Bilal,Masud Jehanzeb,Akhtar Suhail
Abstract
Purpose
This paper aims to present a literature review on analytical research on the prediction of aircraft spin and recovery characteristics, as it progressed from the early years of aviation to current state of the art spin technologies.
Design/methodology/approach
Aerodynamic model development approaches that have been generally used in past spin studies are presented. Past contributions in application of these analytical techniques to predict spin and recovery characteristics on various fighters, general aviation and airliners are discussed, thus providing useful reference for researchers embarking aircraft spin research. An overview of the development of spin prevention and spin recovery technologies to mitigate stall/spin susceptibility is presented.
Findings
The challenges associated with the presented techniques that prompt possible future research directions are discussed.
Originality/value
Despite considerable progress in the recent years, no comprehensive review on the analytical and computational research techniques to predict aircraft post-stall/ spin characteristics has been undertaken in the recent years.
Reference67 articles.
1. Aircraft dynamics at high incidence flight with account of unsteady aerodynamic effects,2004
2. Pushing ahead-SUPRA airplane model for upset recovery,2012
3. The influence of reduced reynolds number on the wake of the DrivAer estate vehicle;Journal of Wind Engineering and Industrial Aerodynamics,2019
4. Bifurcation analysis of a highly augmented aircraft model;Journal of Guidance, Control, and Dynamics,1997
5. Characteristics of wings L-Rectangular Clark Y monoplane wing,1935
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