NASA NTRS · 20010106501
Generic Wing-Body Aerodynamics Data Base
Abstract
The wing-body aerodynamics data base consists of a series of CFD (Computational Fluid Dynamics) simulations about a generic wing body configuration consisting of a ogive-circular-cylinder fuselage and a simple symmetric wing mid-mounted on the fuselage. Solutions have been obtained for Nonlinear Potential (P), Euler (E) and Navier-Stokes (N) solvers over a range of subsonic and transonic Mach numbers and angles of attack. In addition, each solution has been computed on a series of grids, coarse, medium and fine to permit an assessment of grid refinement errors.
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Holst, Terry L., Olsen, Thomas H., Kwak, Dochan. 2001-05-21. Generic Wing-Body Aerodynamics Data Base. https://ntrs.nasa.gov/citations/20010106501
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