Author: National Aeronautics and Space Administration (NASA)Publisher: Createspace Independent Publishing Platform
ISBN: 9781724984913
Category :
Languages : en
Pages : 36
Book Description
The dynamic stability and control characteristics of a four-engine turbofan transport model having an upper-surface blown jet flap were investigated by means of the free-flight technique in the Langley full-scale tunnel. The flight characteristics of the model were investigated through a range of lift coefficients from 3 to 8 with all four engines operating and with one outboard engine not operating. Static characteristics were investigated by conventional power-on force tests over the flight-test angle-of-attack range and through the stall. Parlett, L. P. Langley Research Center NASA-TN-D-8479, L-11332 RTOP 505-11-16-11...
Author: Lysle P. Parlett
Author: Lysle P. Parlett
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Author: Chuan-Tau Edward Lan