The Estimation of Tail Loading Due to Elevator‐Induced Pitching Manoeuvres: A Proposal for an Approximate Analytical Method for Airworthiness Calculations PART III — Appendices

Abstract

This Part presents Appendices I and II which deal, respectively, with the theoretical analysis of the checked manoeuvre and a new simplified method of determining flight loads to cover all pitching manoeuvres, in a form suitable for amendment of civil airworthiness regulations. The latter method also considers additional design cases, including the loading conditions arising from the malfunctioning of an anto‐pilot in pitch: a specimen calculation is also given.

Citation

Richards, P.F. (1960), "The Estimation of Tail Loading Due to Elevator‐Induced Pitching Manoeuvres: A Proposal for an Approximate Analytical Method for Airworthiness Calculations PART III — Appendices", Aircraft Engineering and Aerospace Technology, Vol. 32 No. 3, pp. 77-84. https://doi.org/10.1108/eb033222