Thrust/drag decomposition using partial pressure fields
| dc.contributor.author | Hart, Pierce L. | |
| dc.contributor.author | Mutangara, Ngonidzashe E. | |
| dc.contributor.author | Sanders, Drewan S. | |
| dc.contributor.author | Schmitz, Sven | |
| dc.date.accessioned | 2023-05-17T15:24:04Z | |
| dc.date.available | 2023-05-17T15:24:04Z | |
| dc.date.issued | 2023-03-31 | |
| dc.description | Presented at: 57th 3AF Applied Aerodynamics Conference AERO2023, 29-31 March 2023, Bordeaux, France | |
| dc.description.abstract | The accurate prediction of aircraft performance requires a robust definition of thrust/drag accounting. Traditional nacelle-pylon configurations have been treated as separate entities which are combined linearly; however, this is not feasible for embedded propulsion systems which have a higher degree of interaction than traditional designs. With the apparent shift to embedded propulsion systems in the N+3 generation of aircraft, of which boundary layer ingestion technology is a driving factor, improving our understanding of propulsion system interactions with an air-frame has never been more important. Since many of these interactions occur close to the body, a near-field decomposition method, partial pressure fields, is employed in CFD to provide insight as to the interactive aerodynamics of an embedded propulsion system. | en_UK |
| dc.identifier.citation | Hart PI, Mutangara NE, Sanders DS, Schmitz S. (2023) Thrust/drag decomposition using partial pressure fields. In: 57th 3AF Applied Aerodynamics Conference AERO2023, 29-31 March 2023, Bordeaux, France | en_UK |
| dc.identifier.uri | https://dspace.lib.cranfield.ac.uk/handle/1826/19663 | |
| dc.language.iso | en | en_UK |
| dc.publisher | Association Aeronautique et Astronautique de France (3AF) | en_UK |
| dc.rights | Attribution 4.0 International | * |
| dc.rights.uri | http://creativecommons.org/licenses/by/4.0/ | * |
| dc.title | Thrust/drag decomposition using partial pressure fields | en_UK |
| dc.type | Conference paper | en_UK |