Damaged airplane flight envelope and stability evaluation

Abstract

Purpose

Understanding the performance and flight envelope of a damaged aircraft is a preliminary requirement to recover the aircraft after damage. This paper aims to provide a comprehensive understanding of wing damage effect on airplane performance, local stability, and flying quality of each trim state inside the achievable flight envelope.

Design/methodology/approach

This paper demonstrates the use of attainable equilibrium points which are referred as trim states in order to estimate a damaged airplane manoeuvring flight envelope using a numerical computation method.

Findings

Wing damaged airplane manoeuvring flight envelope is estimated for different portions of the wing tip loss. Local stability at each trim condition inside the estimated flight envelope is analysed, and also motion flight modes and flying quality sensitivity to the wing damage are explored.

Originality/value

Local stability and flying quality analysis at each trim condition inside the flight envelope which demonstrate the effect of damage provides a criterion to prioritize the choice of trimmed flight condition as motion primitives for the airplane post‐damage flight and safe landing.

Citation

Asadi, D., Sabzehparvar, M. and Talebi, H.A. (2013), "Damaged airplane flight envelope and stability evaluation", Aircraft Engineering and Aerospace Technology, Vol. 85 No. 3, pp. 186-198. https://doi.org/10.1108/00022661311313623