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Generic Wing-Body Aerodynamics Data BaseThe 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.
Document ID
20010106501
Acquisition Source
Ames Research Center
Document Type
Other
Authors
Holst, Terry L. (NASA Ames Research Center Moffett Field, CA United States)
Olsen, Thomas H. (NASA Ames Research Center Moffett Field, CA United States)
Kwak, Dochan
Date Acquired
August 20, 2013
Publication Date
May 21, 2001
Subject Category
Aircraft Design, Testing And Performance
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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