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NASA NTRS ยท 19890007381

Computational methods for inlet airframe integration

Abstract

Fundamental equations encountered in computational fluid dynamics (CFD), and analyses used for internal flow are introduced. Irrotational flow; Euler equations; boundary layers; parabolized Navier-Stokes equations; and time averaged Navier-Stokes equations are treated. Assumptions made and solution methods are outlined, with examples. The overall status of CFD in propulsion is indicated.

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BibTeXRIS

Towne, Charles E.. 1988-01-01. Computational methods for inlet airframe integration. https://ntrs.nasa.gov/citations/19890007381

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