NASA NTRS · 19870000548
Computing Aerodynamics Of Propfans
Abstract
Cost and duration of wind-tunnel tests reduced. Computer program developed to predict interference of slipstream of propfan on supercritical wing at subsonic speeds. Use of program reduces cost and time involved in wind-tunnel testing of newly-designed wing/nacelle configurations. Program written in FORTRAN V.
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Chandrasekaran, B.. 1987-11-01. Computing Aerodynamics Of Propfans. https://ntrs.nasa.gov/citations/19870000548
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