A Low Cost Stall/Spin Simulator

A method for simulating flight conditions into stall, post-stall spin entry and steady state spin has been developed using a high performance graphics workstation. Its objective is to provide an easy and low cost means of evaluating the high angular rate and high angle of attack handling qualities o...

Ausführliche Beschreibung

Bibliographische Detailangaben

Veröffentlicht in:	SAE transactions 1989-01, Vol.98, p.107-113
1. Verfasser:	Nagati, M. G.
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Aircraft Aircraft wings Angular velocity Coordinate systems Equations of motion Light aircraft Planforms Polygons Sine function
Online-Zugang:	Volltext
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