NASA NTRS · 19800034065
Experimental and computational study of transonic flow about swept wings
Abstract
An experimental investigation of NACA 0010 and 10% circular arc wing models, swept at 45 deg, spanning a channel, and at zero angle of attack is described. Measurements include chordwise and spanwise surface pressure distributions and oil-flow patterns for a range of transonic Mach numbers and Reynolds numbers. Calculations using a new three-dimensional Navier-Stokes code and a two-equation turbulence model are included for the circular-arc wing flow. Reasonable agreement between measurements and computations is obtained.
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Bertelrud, A., Bergmann, M. Y., Coakley, T. J.. 1980-01-01. Experimental and computational study of transonic flow about swept wings. https://ntrs.nasa.gov/citations/19800034065
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