Investigation the performance of synthetic jet actuator driven by piezoelectric diaphragm for flow separation

Also available in printed version

Détails bibliographiques
Auteur principal: Samaladewi Murukappan
Autres auteurs: Md. Nizam Dahalan, supervisor
Format: Bachelor thesis
Langue:anglais
Publié: Universiti Teknologi Malaysia 2025
Sujets:
Accès en ligne:https://utmik.utm.my/handle/123456789/42857
Abstract Abstract here
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author Samaladewi Murukappan
author2 Md. Nizam Dahalan, supervisor
author_facet Md. Nizam Dahalan, supervisor
Samaladewi Murukappan
author_sort Samaladewi Murukappan
description Also available in printed version
format Bachelor thesis
id utm-123456789-42857
institution Universiti Teknologi Malaysia
language English
publishDate 2025
publisher Universiti Teknologi Malaysia
record_format dspace
record_pdf Abstract
spelling utm-123456789-428572025-08-20T19:09:30Z Investigation the performance of synthetic jet actuator driven by piezoelectric diaphragm for flow separation Samaladewi Murukappan Md. Nizam Dahalan, supervisor Mechanical engineering Also available in printed version Synthetic jet actuator is an active flow control device that used to delay the flow separation and improves the aerodynamic performance such as the wing of an aircraft. The objective of this study is to investigate the performance of synthetic jet actuator design for flow separation with the effect of various orifice depth, cavity thickness and the number of piezoelectric diaphragms using experimental method. There are seven models of synthetic jet actuators were designed, fabricated and testing. Three of the models have different orifice depth and four models built up with various cavity thickness. The experiments were conducted by single and dual piezoelectric diaphragms. A hot-wire anemometer is used to determine the exit air jet velocity through the orifice. The main outcomes of the experiments are to identify the maximum exit air jet velocity and turbulence intensities on different applied frequencies for both single and dual diaphragms. The results show that the exit air jet velocity increases better if the orifice depth reduced and the cavity thickness is smaller. And the best performance of the synthetic jet actuator is identified on the piezoelectric dual diaphragms. shafika UTM 125 p. Kertas Projek (Sarjana Muda Kejuruteraan (Aeronautik)) - Universiti Teknologi Malaysia, 2020 2025-03-11T05:20:49Z 2025-03-11T05:20:49Z 2020 Bachelor thesis https://utmik.utm.my/handle/123456789/42857 vital:149012 valet-20221108-132627 ENG Closed Access UTM Complete Unpublished Completion application/pdf Universiti Teknologi Malaysia
spellingShingle Mechanical engineering
Samaladewi Murukappan
Investigation the performance of synthetic jet actuator driven by piezoelectric diaphragm for flow separation
thesis_level Other
title Investigation the performance of synthetic jet actuator driven by piezoelectric diaphragm for flow separation
title_full Investigation the performance of synthetic jet actuator driven by piezoelectric diaphragm for flow separation
title_fullStr Investigation the performance of synthetic jet actuator driven by piezoelectric diaphragm for flow separation
title_full_unstemmed Investigation the performance of synthetic jet actuator driven by piezoelectric diaphragm for flow separation
title_short Investigation the performance of synthetic jet actuator driven by piezoelectric diaphragm for flow separation
title_sort investigation the performance of synthetic jet actuator driven by piezoelectric diaphragm for flow separation
topic Mechanical engineering
url https://utmik.utm.my/handle/123456789/42857
work_keys_str_mv AT samaladewimurukappan investigationtheperformanceofsyntheticjetactuatordrivenbypiezoelectricdiaphragmforflowseparation