Show simple item record

contributor authorQitai Eri; Liang Hong; Ting Li
date accessioned2019-03-10T11:58:18Z
date available2019-03-10T11:58:18Z
date issued2019
identifier other%28ASCE%29AS.1943-5525.0000936.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4254572
description abstractA novel piston-type synthetic jet actuator (SJA) is developed which has an auxiliary air inlet close to bottom dead center (BDC) to alleviate the difficulty during suction duration. The flow characteristics of the novel SJA are studied numerically and experimentally. The effects of the orifice diameter, actuation frequency, and height of the auxiliary air inlet on the actuator performance are also analyzed. The results indicate that the auxiliary air inlet significantly improves the performance of the SJA, especially for small orifices and high actuation frequencies. Compared with the conventional piston-type SJA, the mass flow of the novel SJA is increased significantly, which is the major reason for the increase in cylinder pressure, maximum jet momentum, duty cycle, and efficiency of the actuator.
publisherAmerican Society of Civil Engineers
titleNovel Piston-Type Synthetic Jet Actuator with Auxiliary Air Inlet
typeJournal Paper
journal volume32
journal issue1
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)AS.1943-5525.0000936
page04018127
treeJournal of Aerospace Engineering:;2019:;Volume ( 032 ):;issue: 001
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record