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 : https://apps.dtic.mil/dtic/tr/fulltext/u2/1045805.pdf


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