Accession Number : AD1045805

Title :   Pressure Scalings and Influence Region Research

Descriptive Note : Technical Report,01 Jul 2015,01 Jan 2018

Corporate Author : Air Force Research Laboratory, Aerospace Systems Directorate Wright-Patterson Air Force Base United States

Personal Author(s) : Miller,James H

Full Text :

Report Date : 01 Jan 2018

Pagination or Media Count : 14

Abstract : An updated non-dimensional approach for pressure is used to normalize the Navier-Stokes equations and the results are briefly discussed. Additionally, updated experimental results are presented along with discussion of collaborative research efforts in asymptotic theory and application of computational fluid dynamics (CFD) methods to utilize influence regions to improve computational efficiency when changes in geometry become a significant driver to computational analysis timelines.

Descriptors :   Navier Stokes equations , boundary layer , SUPERSONIC FLOW , COMPUTATIONAL FLUID DYNAMICS , Reynolds number , flow fields

Subject Categories : Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE