NASA NTRS · 19750020940
Computational aerodynamics
Abstract
The application of computer techniques for solving Navier-Stokes equations in support of wind tunnel tests is discussed. The ILLIAC IV computer is considered for this purpose and its limitations are analyzed. The author states that improved computers will make it possible to solve many aerodynamic problems and reduce the amount of wind tunnel testing required for adequate data processing.
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Chapman, D. R.. 1975-01-01. Computational aerodynamics. https://ntrs.nasa.gov/citations/19750020940
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