2026-06-02T05:18:15Zhttps://riuma.uma.es/rest/oai/request

oai:riuma.uma.es:10630/163972026-02-03T12:16:55Zcom_10630_2254col_10630_37959

On the effect of low blowing ratio continuous jets on wingtip vortex characteristics Blanco-Rodríguez, Francisco José Parras-Anguita, Luis Del-Pino-Peñas, Carlos Manuel García Ortiz, José Hermenegildo Vortices are an unavoidable effect of flight, which appear behind the wing with a bounded length. The strength of these vortices, which are extremely stable, is due to the lift force [1]. That is the reason why this phenomenon is especially relevant during take-off and landing operations. In these situations, when aircraft are departing from or arriving to the airport runways, the following aircraft might feel two counter-rotating vortices which remain long time under normal environmental conditions. Unfortunately, this huge rotation of airflow patterns always destabilizes the following aircraft. Consequently, trailing vortices have a mighty influence on the air traffic control of airport runways, and they have justified the research interest in this topic since the 1960's [2]. However, aeronautical engineers are still searching for different technological strategies to breakdown these wingtip vortices. 2018-09-03T11:06:15Z 2018-09-03T11:06:15Z 2018-07-11 2018-09-03 conference output https://hdl.handle.net/10630/16397 eng 7th Conference on Bluff Body Wakes and Vortex-Induced Vibrations Carry-le-Rouet (Marseille), FRANCE 3-6 Julio 2018 open access