CFD analyses of the P-3C Orion (Aurora)

DOI	Trouver le DOI : https://doi.org/10.2514/6.2000-127
Auteur	Rechercher : Kumar, Sanjiv¹; Rechercher : Fortin, Francois¹; Rechercher : Benmeddour, Ali¹
Affiliation	Conseil national de recherches du Canada. Institut de recherche aérospatiale du CNRC
Format	Texte, Article
Conférence	38th Aerospace Sciences Meeting and Exhibit, January 10-13, 2000, Reno, NV, USA
Résumé	An unstructured Euler solver is used to compute flow past the P-3C Orion aircraft (known in Canada as the Aurora). The results of the computation are compared with the available experimental data to assess the code prediction capability. The solver is then used to compute the flow field on a 1:16 scale model with an objective to assess the sting mounting effects on the surface pressure distribution. Computations are made for the model in the free stream, in the wind tunnel without the sting and in the wind tunnel with the sting. These computations provide an assessment of the sting effects which will be used to adjust the experimental results.
Date de publication	2000-01-10
Maison d’édition	American Institute of Aeronautics and Astronautics
Dans	38th Aerospace Sciences Meeting and Exhibit.
Langue	anglais
Publications évaluées par des pairs	Oui
Numéro NPARC	23001670
Exporter la notice	Exporter en format RIS
Signaler une correction	Signaler une correction (s'ouvre dans un nouvel onglet)
Identificateur de l’enregistrement	6fb83519-bdc5-4edc-86ce-20159be32efb
Enregistrement créé	2017-03-16
Enregistrement modifié	2020-03-26