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

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.