Download Development of Direct-Inverse 3-D Methods for Applied Transonic Aerodynamic Wing Design and Analysis - National Aeronautics and Space Administration file in PDF Online

Read Online Development of Direct-Inverse 3-D Methods for Applied Transonic Aerodynamic Wing Design and Analysis - National Aeronautics and Space Administration file in PDF

An inverse wing design method was developed around an existing transonic wing analysis code. The original analysis code, TAWFIVE, has as its core the numerical potential flow solver, FLO30, developed by Jameson and Caughey. Features of the analysis code include a finite-volume formulation; wing and fuselage fitted, curvilinear grid mesh; and a viscous boundary layer

Title : Development of Direct-Inverse 3-D Methods for Applied Transonic Aerodynamic Wing Design and Analysis
Author : National Aeronautics and Space Administration
Language : en
Rating :
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Type : PDF, ePub, Kindle
Uploaded : Apr 06, 2021

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