NASA Technical Reports Server (NTRS) : Methodology pdf

NASA Technical Reports Server (NTRS) : Methodology

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Correction factor methodologies have been developed which use steady experimental or analytical pressure or force data to correct steady and unsteady aerodynamic calculations. Three methods of calculating correction factors have been developed to match steady surface pressure distributions, to match airfoil section forces and moments. Data for a rectangular supercritical wing that was previously tested in the NASA Langley Research Center Transonic Dynamics Tunnel have been used to determine correction factors to match surface pressure distributions for a range of Mach numbers

• Creator/s: NASA Technical Reports Server (NTRS
• Date: 5/1/1988
• Year: 1988
• Book Topics/Themes: NASA Technical Reports Server (NTRS), COMPUTATIONAL FLUID DYNAMICS, PRESSURE DISTRIBUTION, UNSTEADY AERODYNAMICS, WIND TUNNEL TESTS, WING LOADING, COMPUTATIONAL GRIDS, DOWNWASH, RECTANGULAR WINGS, SPLINE FUNCTIONS, SUPERCRITICAL WINGS, Wieseman, Carol D

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