2026-05-27T04:42:45Zhttps://riuma.uma.es/rest/oai/request

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

Blanco-Rodríguez, Francisco José Parras-Anguita, Luis Del-Pino-Peñas, Carlos Manuel García Ortiz, José Hermenegildo 2018-09-03T11:06:15Z 2018-09-03T11:06:15Z 2018-09-03 https://hdl.handle.net/10630/16397 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. eng open access On the effect of low blowing ratio continuous jets on wingtip vortex characteristics conference output