01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
EFFECT OF ENGINE RESPONSE TIME IN AIRCRAFT CONCEPTUAL DESIGN
A.P.S. Inderawan¹, M. Hoogreef¹; ¹Delft University of Technology, Netherlands
Engine response time is not something typically considered early in aircraft conceptual design. In this study, by incorporating engine response time, we propose a method of constructing a go-around constraint curve that also addresses therndecision height as the operational limit. This method ensures that safety of operation of aircraft with novel engine options are considered from the early stage.
DOI: 10.71945/icas2026_0293