A unified partial pressure field and velocity decomposition approach toward improved energetic aerodynamic force decompositions

dc.contributor.authorMutangara, Ngonidzashe E.
dc.contributor.authorSanders, Drewan S.
dc.contributor.authorLaskaridis, Panagiotis
dc.contributor.authorHart, Pierce L.
dc.contributor.authorSchmitz, Sven
dc.date.accessioned2023-05-17T15:44:30Z
dc.date.available2023-05-17T15:44:30Z
dc.date.issued2023-03-31
dc.description.abstractDrag decomposition through energy and exergy-based methods has been shown to have a variety of advantages. One of these is identifying and quantifying the recoverable energy within a flow field. This describes the available energy that can be used to produce thrust through systems such as boundary layer ingestion. Another advantage highlighted from prior work is that the velocity decomposition approach can split the flow field into its isentropic and non-isentropic contributions. This provides region-specific formulations for drag assessment, wherein the isentropic field is associated with contributions originating from the bulk flow and the non-isentropic field with the shear layer. This paper aims to assess the performance of a modified form of the velocity decomposition approach for transonic flows. This modification involves unification with partial pressure field analysis, which provides better flow field separability due to the added decomposition of the pressure field.en_UK
dc.identifier.citationMutangara NE, Sanders DS, Laskaridis P, et al., (2023) A unified partial pressure field and velocity decomposition approach toward improved energetic aerodynamic force decompositions. In: 57th 3AF Applied Aerodynamics Conference AERO2023, 29-31 March 2023, Bordeaux, Franceen_UK
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/19664
dc.language.isoenen_UK
dc.publisherAssociation Aeronautique et Astronautique de France (3AF)en_UK
dc.rightsAttribution 4.0 International*
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/*
dc.titleA unified partial pressure field and velocity decomposition approach toward improved energetic aerodynamic force decompositionsen_UK
dc.typeConference paperen_UK

Files

Original bundle
Now showing 1 - 1 of 1
Loading...
Thumbnail Image
Name:
AERO2023-17-MUTANGARA-2023.pdf
Size:
516.05 KB
Format:
Adobe Portable Document Format
Description:
License bundle
Now showing 1 - 1 of 1
No Thumbnail Available
Name:
license.txt
Size:
1.63 KB
Format:
Item-specific license agreed upon to submission
Description: