Title: Use of the flight simulator in the design of a STOL research aircraft
Abstract: Piloted simulator tests on the NASA-Ames Flight Simulator for Advanced Aircraft motion base played a major role in guiding the design of the Modified C-8A 'Buffalo' augmentor wing jet flap STOL research airplane. Design results are presented for the flight control systems, lateral-directional SAS, hydraulic systems, and engine and thrust vector controls. Emphasis is given to lateral control characteristics on STOL landing approach, engine-out control and recovery techniques in the powered-lift regime, and operational flight procedures which affected airplane design.
Publication Year: 1972
Publication Date: 1972-08-07
Language: en
Type: article
Indexed In: ['crossref']
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Cited By Count: 2
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