Feasibility study of its use for speed and flight path control during approach phase made with North American Fighter-bomber having J57-P-21A turbojet engine; design development through wind tunnel program selecting and adjusting exhaust gas patterns; flight test program showed that reverser selected produced adequate reverse thrust, up to 40% of net forward thrust, with small effects on aircraft stability, trim, and handling characteristics.
Development of in-flight modulating type thrust reverser for single engine aircraft
SAE -- Paper
SAE Meeting ; 1960 Thrust reversal
1960
14 pages
Conference paper
English
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DEVELOPMENT OF IN-FLIGHT MODULATING TYPE THRUST REVERSER FOR SINGLE ENGINE AIRCRAFT
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