{"id":5899,"date":"2020-10-08T13:50:11","date_gmt":"2020-10-08T13:50:11","guid":{"rendered":"https:\/\/research.utm.my\/aerolab\/?post_type=project&#038;p=5899"},"modified":"2021-06-21T05:14:13","modified_gmt":"2021-06-21T05:14:13","slug":"current-research","status":"publish","type":"project","link":"https:\/\/research.utm.my\/aerolab\/project\/current-research\/","title":{"rendered":"Current Research"},"content":{"rendered":"<p>[et_pb_section fb_built=&#8221;1&#8243; _builder_version=&#8221;4.9.4&#8243; hover_enabled=&#8221;0&#8243; custom_padding=&#8221;||31px|||&#8221; background_color=&#8221;#8dc7dd&#8221; sticky_enabled=&#8221;0&#8243;][et_pb_row _builder_version=&#8221;3.25&#8243; background_size=&#8221;initial&#8221; background_position=&#8221;top_left&#8221; background_repeat=&#8221;repeat&#8221; width=&#8221;83.6%&#8221; custom_padding=&#8221;|||27px||&#8221;][et_pb_column type=&#8221;4_4&#8243; _builder_version=&#8221;3.25&#8243; custom_padding=&#8221;|||&#8221; custom_padding__hover=&#8221;|||&#8221;][et_pb_text _builder_version=&#8221;3.27.4&#8243; background_size=&#8221;initial&#8221; background_position=&#8221;top_left&#8221; background_repeat=&#8221;repeat&#8221; custom_padding=&#8221;|||20px||&#8221;]<!-- divi:gallery {\"ids\":[5900,5901]} --><\/p>\n<figure class=\"wp-block-gallery columns-2 is-cropped\">\n<ul class=\"blocks-gallery-grid\">\n<li class=\"blocks-gallery-item\">\n<figure>\u00a0<img loading=\"lazy\" decoding=\"async\" width=\"707\" height=\"418\" src=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/BWBmodel.jpg\" alt=\"\" data-id=\"5900\" class=\"wp-image-5900\" srcset=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/BWBmodel.jpg 707w, https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/BWBmodel-480x284.jpg 480w\" sizes=\"(min-width: 0px) and (max-width: 480px) 480px, (min-width: 481px) 707px, 100vw\" \/><\/figure>\n<\/li>\n<li class=\"blocks-gallery-item\">\n<figure><img loading=\"lazy\" decoding=\"async\" width=\"676\" height=\"365\" src=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/BWBmodel2.jpg\" alt=\"\" data-id=\"5901\" data-full-url=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/BWBmodel2.jpg\" data-link=\"https:\/\/research.utm.my\/aerolab\/?attachment_id=5901\" class=\"wp-image-5901\" srcset=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/BWBmodel2.jpg 676w, https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/BWBmodel2-480x259.jpg 480w\" sizes=\"(min-width: 0px) and (max-width: 480px) 480px, (min-width: 481px) 676px, 100vw\" \/><\/figure>\n<\/li>\n<\/ul><figcaption class=\"blocks-gallery-caption\">Blended Wing body research headed by Dr Shabudin bin Mat<\/figcaption><\/figure>\n<p>&nbsp;<\/p>\n<p><!-- \/divi:image -->[\/et_pb_text][\/et_pb_column][\/et_pb_row][\/et_pb_section][et_pb_section fb_built=&#8221;1&#8243; _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; background_color=&#8221;#FFFFFF&#8221; hover_enabled=&#8221;0&#8243; sticky_enabled=&#8221;0&#8243; custom_padding=&#8221;10px||4px|||&#8221;][et_pb_row _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221;][et_pb_column _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; type=&#8221;4_4&#8243;][et_pb_text _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; hover_enabled=&#8221;0&#8243; sticky_enabled=&#8221;0&#8243; custom_padding=&#8221;1px||20px|||&#8221;]<\/p>\n<p>&nbsp;<\/p>\n<p>&nbsp;<\/p>\n<p><!-- divi:image {\"align\":\"center\",\"id\":5902,\"sizeSlug\":\"large\"} --><\/p>\n<div class=\"wp-block-image\">\n<figure class=\"aligncenter size-large\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/synthetic-jet-actuator.png\" alt=\"\" class=\"wp-image-5902\" width=\"463\" height=\"261\" style=\"margin-left: auto;margin-right: auto\" \/><\/p>\n<p><span style=\"font-size: 14px\">\u00a0<\/span><span style=\"font-size: 14px\">\u00a0<\/span><span style=\"font-size: 14px\">\u00a0<\/span><span style=\"font-size: 14px\">Experiment on Synthetic jet actuators performance &#8211; Research headed by Dr Nizam Dahalan<\/span><\/p>\n<\/figure>\n<\/div>\n<p>[\/et_pb_text][\/et_pb_column][\/et_pb_row][\/et_pb_section][et_pb_section fb_built=&#8221;1&#8243; _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; background_color=&#8221;#88C4DD&#8221; hover_enabled=&#8221;0&#8243; sticky_enabled=&#8221;0&#8243; custom_padding=&#8221;||4px|||&#8221;][et_pb_row _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221;][et_pb_column _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; type=&#8221;4_4&#8243;][et_pb_text _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; hover_enabled=&#8221;0&#8243; sticky_enabled=&#8221;0&#8243;]<\/p>\n<ul class=\"blocks-gallery-grid\">\n<li class=\"blocks-gallery-item\">\n<figure><img loading=\"lazy\" decoding=\"async\" width=\"1024\" height=\"443\" src=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/composite2-1024x443.png\" alt=\"\" data-id=\"5905\" data-full-url=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/composite2.png\" data-link=\"https:\/\/research.utm.my\/aerolab\/?attachment_id=5905\" class=\"wp-image-5905\" srcset=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/composite2-1024x443.png 1024w, https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/composite2-980x424.png 980w, https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/composite2-480x208.png 480w\" sizes=\"(min-width: 0px) and (max-width: 480px) 480px, (min-width: 481px) and (max-width: 980px) 980px, (min-width: 981px) 1024px, 100vw\" \/><\/figure>\n<\/li>\n<\/ul>\n<p style=\"text-align: center\">Coreless Spoiler structure analysis &#8211; Research headed by Dr Haris Ahmad Israr Ahmad and Associate Professor Ainullotfi bin Abdul Latif<\/p>\n<p>[\/et_pb_text][\/et_pb_column][\/et_pb_row][\/et_pb_section][et_pb_section fb_built=&#8221;1&#8243; _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; custom_padding=&#8221;5px||11px|||&#8221; background_color=&#8221;#FFFFFF&#8221; hover_enabled=&#8221;0&#8243; sticky_enabled=&#8221;0&#8243;][et_pb_row _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221;][et_pb_column _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; type=&#8221;4_4&#8243;][et_pb_text _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; hover_enabled=&#8221;0&#8243; sticky_enabled=&#8221;0&#8243;]<\/p>\n<ul class=\"blocks-gallery-grid\">\n<li class=\"blocks-gallery-item\">\n<figure><img loading=\"lazy\" decoding=\"async\" width=\"424\" height=\"318\" src=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/helicopter-1.jpg\" alt=\"\" data-id=\"5907\" class=\"wp-image-5907\" srcset=\"https:\/\/research.utm.my\/aerolab\/wp-content\/uploads\/sites\/50\/2020\/10\/helicopter-1.jpg 424w, https:\/\/research.utm.my\/aerolab\/wp-content\/uploads\/sites\/50\/2020\/10\/helicopter-1-300x225.jpg 300w\" sizes=\"(max-width: 424px) 100vw, 424px\" \/><\/figure>\n<\/li>\n<li class=\"blocks-gallery-item\">\n<figure><img loading=\"lazy\" decoding=\"async\" width=\"344\" height=\"172\" src=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/helicopter2-1.png\" alt=\"\" data-id=\"5909\" data-full-url=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/helicopter2-1.png\" data-link=\"https:\/\/research.utm.my\/aerolab\/?attachment_id=5909\" class=\"wp-image-5909\" style=\"margin-left: auto;margin-right: auto\" srcset=\"https:\/\/research.utm.my\/aerolab\/wp-content\/uploads\/sites\/50\/2020\/10\/helicopter2-1.png 344w, https:\/\/research.utm.my\/aerolab\/wp-content\/uploads\/sites\/50\/2020\/10\/helicopter2-1-300x150.png 300w\" sizes=\"(max-width: 344px) 100vw, 344px\" \/><\/figure>\n<\/li>\n<\/ul>\n<p style=\"text-align: center\">Helicopter Tail Shake Phenomenon experiment &#8211; Research headed by Dr Iskandar Shah Ishak<\/p>\n<p>[\/et_pb_text][\/et_pb_column][\/et_pb_row][\/et_pb_section][et_pb_section fb_built=&#8221;1&#8243; _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; custom_padding=&#8221;13px||0px|||&#8221; background_color=&#8221;#88C4DD&#8221; hover_enabled=&#8221;0&#8243; sticky_enabled=&#8221;0&#8243;][et_pb_row _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221;][et_pb_column _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; type=&#8221;4_4&#8243;][et_pb_text _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; hover_enabled=&#8221;0&#8243; sticky_enabled=&#8221;0&#8243;]<\/p>\n<ul class=\"blocks-gallery-grid\">\n<li class=\"blocks-gallery-item\">\n<figure><img loading=\"lazy\" decoding=\"async\" width=\"412\" height=\"248\" src=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/CAMAR3.jpg\" alt=\"\" data-id=\"5910\" class=\"wp-image-5910\" style=\"margin-left: auto;margin-right: auto\" srcset=\"https:\/\/research.utm.my\/aerolab\/wp-content\/uploads\/sites\/50\/2020\/10\/CAMAR3.jpg 412w, https:\/\/research.utm.my\/aerolab\/wp-content\/uploads\/sites\/50\/2020\/10\/CAMAR3-300x181.jpg 300w\" sizes=\"(max-width: 412px) 100vw, 412px\" \/><\/p>\n<p style=\"text-align: center\">\n<p style=\"text-align: center\">\u00a0<\/p>\n<p style=\"text-align: center\">\u00a0<\/p>\n<p style=\"text-align: center\">\u00a0<\/p>\n<p style=\"text-align: center\">\u00a0<\/p>\n<p style=\"text-align: center\">\u00a0<\/p>\n<p style=\"text-align: center\">\u00a0<\/p>\n<p style=\"text-align: center\">\u00a0<\/p>\n<p style=\"text-align: center\">\u00a0<\/p>\n<p style=\"text-align: center\">\u00a0<\/p><figcaption class=\"blocks-gallery-item__caption\">CAMAR III<\/figcaption><\/figure>\n<\/li>\n<li class=\"blocks-gallery-item\" style=\"text-align: center\">\n<figure><img loading=\"lazy\" decoding=\"async\" width=\"1024\" height=\"536\" src=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/flight-testing-2-1024x536.png\" alt=\"\" data-id=\"5921\" data-full-url=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/flight-testing-2.png\" data-link=\"https:\/\/research.utm.my\/aerolab\/?attachment_id=5921\" class=\"wp-image-5921\" srcset=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/flight-testing-2-1024x536.png 1024w, https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/flight-testing-2-980x513.png 980w, https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/flight-testing-2-480x251.png 480w\" sizes=\"(min-width: 0px) and (max-width: 480px) 480px, (min-width: 481px) and (max-width: 980px) 980px, (min-width: 981px) 1024px, 100vw\" \/><\/figure>\n<\/li>\n<\/ul>\n<p style=\"text-align: center\">CAMAR III flight testing &#8211; Research Headed by Dr Mohd Nazri, Prof Ir Dr Shuhaimi Mansor<\/p>\n<p>[\/et_pb_text][\/et_pb_column][\/et_pb_row][\/et_pb_section][et_pb_section fb_built=&#8221;1&#8243; _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; custom_padding=&#8221;3px||2px|||&#8221;][et_pb_row _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; column_structure=&#8221;1_2,1_2&#8243;][et_pb_column _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; type=&#8221;1_2&#8243;][et_pb_text _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; hover_enabled=&#8221;0&#8243; sticky_enabled=&#8221;0&#8243;]<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/CFD1.png\" alt=\"\" class=\"wp-image-5912\" width=\"431\" height=\"384\" \/><\/p>\n<p>[\/et_pb_text][\/et_pb_column][et_pb_column _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; type=&#8221;1_2&#8243;][et_pb_text _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; hover_enabled=&#8221;0&#8243; sticky_enabled=&#8221;0&#8243;]<\/p>\n<p>Vortex induced vibration analysis using CFD &#8211; Research headed by Dr Nik Ahmad Ridhwan<\/p>\n<p>[\/et_pb_text][\/et_pb_column][\/et_pb_row][\/et_pb_section][et_pb_section fb_built=&#8221;1&#8243; _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; background_color=&#8221;#88C4DD&#8221; hover_enabled=&#8221;0&#8243; sticky_enabled=&#8221;0&#8243; custom_padding=&#8221;2px||0px|||&#8221;][et_pb_row _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; column_structure=&#8221;1_2,1_2&#8243;][et_pb_column _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; type=&#8221;1_2&#8243;][et_pb_image src=&#8221;https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/propeller-testing.jpg&#8221; _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; title_text=&#8221;propeller-testing&#8221; hover_enabled=&#8221;0&#8243; sticky_enabled=&#8221;0&#8243; height=&#8221;552px&#8221; module_alignment=&#8221;center&#8221; width=&#8221;61%&#8221;][\/et_pb_image][et_pb_text _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; hover_enabled=&#8221;0&#8243; sticky_enabled=&#8221;0&#8243;]<\/p>\n<figure style=\"text-align: center\"><figcaption class=\"blocks-gallery-item__caption\">Propeller performance testing<\/figcaption><\/figure>\n<figure><\/figure>\n<p>[\/et_pb_text][\/et_pb_column][et_pb_column _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; type=&#8221;1_2&#8243;][et_pb_image src=&#8221;https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/VTOL-1.png&#8221; _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; title_text=&#8221;VTOL-1&#8243; module_alignment=&#8221;center&#8221; width=&#8221;91%&#8221; min_height=&#8221;372px&#8221; hover_enabled=&#8221;0&#8243; sticky_enabled=&#8221;0&#8243;][\/et_pb_image][et_pb_text _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; hover_enabled=&#8221;0&#8243; sticky_enabled=&#8221;0&#8243;]<\/p>\n<figure style=\"text-align: center\"><figcaption class=\"blocks-gallery-item__caption\">Conceptual VTOL design<\/figcaption><\/figure>\n<p>[\/et_pb_text][\/et_pb_column][\/et_pb_row][et_pb_row _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; custom_padding=&#8221;||23px|||&#8221;][et_pb_column _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; type=&#8221;4_4&#8243;][et_pb_text _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; hover_enabled=&#8221;0&#8243; sticky_enabled=&#8221;0&#8243;]<\/p>\n<figure class=\"wp-block-gallery columns-2 is-cropped\" style=\"text-align: left\"><figcaption class=\"blocks-gallery-caption\">UAV VTOL design and development. Propeller performance analysis and obstacle avoidance design<br \/>Research headed by Dr Mastura Ab Wahid<\/figcaption><\/figure>\n<p style=\"text-align: center\">[\/et_pb_text][\/et_pb_column][\/et_pb_row][\/et_pb_section][et_pb_section fb_built=&#8221;1&#8243; _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221;][et_pb_row column_structure=&#8221;1_2,1_2&#8243; _builder_version=&#8221;4.6.5&#8243; _module_preset=&#8221;default&#8221;][et_pb_column type=&#8221;1_2&#8243; _builder_version=&#8221;4.6.5&#8243; _module_preset=&#8221;default&#8221;][et_pb_image src=&#8221;https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/greencombustion.jpeg&#8221; title_text=&#8221;greencombustion&#8221; _builder_version=&#8221;4.6.5&#8243; _module_preset=&#8221;default&#8221;][\/et_pb_image][\/et_pb_column][et_pb_column type=&#8221;1_2&#8243; _builder_version=&#8221;4.6.5&#8243; _module_preset=&#8221;default&#8221;][et_pb_image src=&#8221;https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/gasifier.jpeg&#8221; title_text=&#8221;gasifier&#8221; _builder_version=&#8221;4.6.5&#8243; _module_preset=&#8221;default&#8221;][\/et_pb_image][et_pb_image src=&#8221;https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/microturbine.jpeg&#8221; title_text=&#8221;microturbine&#8221; _builder_version=&#8221;4.6.5&#8243; _module_preset=&#8221;default&#8221;][\/et_pb_image][et_pb_text _builder_version=&#8221;4.6.5&#8243; _module_preset=&#8221;default&#8221;]<\/p>\n<p>Figure above (a) gasifier system (b) gas turbine system<\/p>\n<p>This green technology is headed by Prof Dr Nazri Jaafar. members: PM Dr Tholudin, Dr Wan Zaidi, Dr Norazila<\/p>\n<p>[\/et_pb_text][\/et_pb_column][\/et_pb_row][\/et_pb_section][et_pb_section fb_built=&#8221;1&#8243; _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; background_color=&#8221;#88C4DD&#8221; hover_enabled=&#8221;0&#8243; sticky_enabled=&#8221;0&#8243; custom_padding=&#8221;0px||7px|||&#8221;][et_pb_row column_structure=&#8221;1_2,1_2&#8243; _builder_version=&#8221;4.6.5&#8243; _module_preset=&#8221;default&#8221;][et_pb_column type=&#8221;1_2&#8243; _builder_version=&#8221;4.6.5&#8243; _module_preset=&#8221;default&#8221;][et_pb_image src=&#8221;https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/tedung-kilat.jpg&#8221; title_text=&#8221;tedung-kilat&#8221; _builder_version=&#8221;4.6.5&#8243; _module_preset=&#8221;default&#8221;][\/et_pb_image][et_pb_image src=&#8221;https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/temperature-distribution-inside-chamber.jpeg&#8221; title_text=&#8221;temperature distribution inside chamber&#8221; _builder_version=&#8221;4.6.5&#8243; _module_preset=&#8221;default&#8221;][\/et_pb_image][\/et_pb_column][et_pb_column type=&#8221;1_2&#8243; _builder_version=&#8221;4.6.5&#8243; _module_preset=&#8221;default&#8221;][et_pb_image src=&#8221;https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/50N-thruster.jpeg&#8221; title_text=&#8221;50N thruster&#8221; _builder_version=&#8221;4.6.5&#8243; _module_preset=&#8221;default&#8221; custom_padding=&#8221;|||84px||&#8221;][\/et_pb_image][et_pb_image src=&#8221;https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/200N-thrust.png&#8221; title_text=&#8221;200N thrust&#8221; _builder_version=&#8221;4.6.5&#8243; _module_preset=&#8221;default&#8221; custom_margin=&#8221;||-1px|||&#8221; custom_padding=&#8221;|178px||||&#8221;][\/et_pb_image][\/et_pb_column][\/et_pb_row][et_pb_row _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221;][et_pb_column _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; type=&#8221;4_4&#8243;][et_pb_text _builder_version=&#8221;4.6.5&#8243; _module_preset=&#8221;default&#8221; width=&#8221;100%&#8221; custom_padding=&#8221;|||14px||&#8221;]<\/p>\n<p>Tedung kilat launched in 2010 -research headed by Prof Ir Dr Wan Khairuddin.<\/p>\n<p>Pic above 50N thruster liquid propellent. Pic on the left, temperature distribution analysis on rocket body.<\/p>\n<p>Members of the project: Dr Norazila and Dr Mastura<\/p>\n<p>[\/et_pb_text][\/et_pb_column][\/et_pb_row][\/et_pb_section][et_pb_section fb_built=&#8221;1&#8243; _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; custom_padding=&#8221;1px|||||&#8221;][et_pb_row column_structure=&#8221;1_2,1_2&#8243; _builder_version=&#8221;4.6.5&#8243; _module_preset=&#8221;default&#8221;][et_pb_column type=&#8221;1_2&#8243; _builder_version=&#8221;4.6.5&#8243; _module_preset=&#8221;default&#8221;][et_pb_image src=&#8221;https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/turbinedesign.jpeg&#8221; title_text=&#8221;turbinedesign&#8221; _builder_version=&#8221;4.6.5&#8243; _module_preset=&#8221;default&#8221;][\/et_pb_image][\/et_pb_column][et_pb_column type=&#8221;1_2&#8243; _builder_version=&#8221;4.6.5&#8243; _module_preset=&#8221;default&#8221;][et_pb_image src=&#8221;https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/otec-cycle.jpeg&#8221; title_text=&#8221;otec cycle&#8221; _builder_version=&#8221;4.6.5&#8243; _module_preset=&#8221;default&#8221; custom_margin=&#8221;||-10px|||&#8221;][\/et_pb_image][et_pb_text _builder_version=&#8221;4.6.5&#8243; _module_preset=&#8221;default&#8221; custom_padding=&#8221;18px||32px|||&#8221;]<\/p>\n<p>Above is the OTEC cycle system. On the left is the turbine design.<\/p>\n<p>\u00a0This is a project under Ocean Thermal Energy Conversion (OTEC) team. Headed by Prof Ir. Dr. Shuhaimi Mansor.\u00a0<\/p>\n<p>[\/et_pb_text][\/et_pb_column][\/et_pb_row][\/et_pb_section][et_pb_section fb_built=&#8221;1&#8243; _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; background_color=&#8221;#88C4DD&#8221; hover_enabled=&#8221;0&#8243; sticky_enabled=&#8221;0&#8243; custom_padding=&#8221;0px|||||&#8221;][et_pb_row column_structure=&#8221;1_2,1_2&#8243; _builder_version=&#8221;4.6.5&#8243; _module_preset=&#8221;default&#8221; custom_padding=&#8221;|||86px||&#8221;][et_pb_column type=&#8221;1_2&#8243; _builder_version=&#8221;4.6.5&#8243; _module_preset=&#8221;default&#8221;][et_pb_image src=&#8221;https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/istas1.jpg&#8221; title_text=&#8221;istas1&#8243; _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; custom_margin=&#8221;|100px||||&#8221; custom_padding=&#8221;|17px||||&#8221; hover_enabled=&#8221;0&#8243; align=&#8221;center&#8221; sticky_enabled=&#8221;0&#8243;][\/et_pb_image][\/et_pb_column][et_pb_column type=&#8221;1_2&#8243; _builder_version=&#8221;4.6.5&#8243; _module_preset=&#8221;default&#8221;][et_pb_image src=&#8221;https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/data-analytics.jpg&#8221; title_text=&#8221;data analytics&#8221; _builder_version=&#8221;4.6.5&#8243; _module_preset=&#8221;default&#8221;][\/et_pb_image][\/et_pb_column][\/et_pb_row][et_pb_row _builder_version=&#8221;4.6.5&#8243; _module_preset=&#8221;default&#8221; custom_padding=&#8221;|||10px||&#8221;][et_pb_column type=&#8221;4_4&#8243; _builder_version=&#8221;4.6.5&#8243; _module_preset=&#8221;default&#8221;][et_pb_text _builder_version=&#8221;4.6.5&#8243; _module_preset=&#8221;default&#8221;]<\/p>\n<p>Flight Simulator and Data analytics to analyse on the information of traffic flow on air and sea.\u00a0<\/p>\n<p>Research headed by Ir Dr Istas Fahrurrazi Nusyriwan<\/p>\n<p>[\/et_pb_text][\/et_pb_column][\/et_pb_row][\/et_pb_section][et_pb_section fb_built=&#8221;1&#8243; _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221;][et_pb_row _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; column_structure=&#8221;1_2,1_2&#8243;][et_pb_column _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; type=&#8221;1_2&#8243;][et_pb_image src=&#8221;https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2021\/06\/Fig-4-scaled.jpg&#8221; _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; title_text=&#8221;Fig 4&#8243; hover_enabled=&#8221;0&#8243; sticky_enabled=&#8221;0&#8243;][\/et_pb_image][\/et_pb_column][et_pb_column _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; type=&#8221;1_2&#8243;][et_pb_image src=&#8221;https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2021\/06\/Fig-41c-scaled.jpg&#8221; _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; title_text=&#8221;Fig 41c&#8221; hover_enabled=&#8221;0&#8243; sticky_enabled=&#8221;0&#8243; align=&#8221;center&#8221; width=&#8221;70%&#8221;][\/et_pb_image][\/et_pb_column][\/et_pb_row][et_pb_row _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221;][et_pb_column _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; type=&#8221;4_4&#8243;][et_pb_text _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; hover_enabled=&#8221;0&#8243; sticky_enabled=&#8221;0&#8243;]<\/p>\n<p>Research on Vibrations, Structural damping, Energy Harvesting, Aerodynamic Flutter. Headed by<\/p>\n<p>Dr Muhammad Faruq Foong bin Mohamad Faiz Foong<\/p>\n<p>[\/et_pb_text][\/et_pb_column][\/et_pb_row][\/et_pb_section][et_pb_section fb_built=&#8221;1&#8243; _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; background_color=&#8221;#C2C2C2&#8243; hover_enabled=&#8221;0&#8243; sticky_enabled=&#8221;0&#8243; custom_padding=&#8221;0px|||||&#8221;][et_pb_row _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221;][et_pb_column _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; type=&#8221;4_4&#8243;][et_pb_text _builder_version=&#8221;4.9.4&#8243; _module_preset=&#8221;default&#8221; hover_enabled=&#8221;0&#8243; sticky_enabled=&#8221;0&#8243; custom_margin=&#8221;31px|||||&#8221;]<\/p>\n<p>If you are interested to know more about the research and wish for collaboration, master research or PhD with us, do not hesitate to contact us. For each PIC you can go to this <a href=\"https:\/\/research.utm.my\/aerolab\/about-us-aerolab\/\">page<\/a>. Thank you<\/p>\n<p>[\/et_pb_text][\/et_pb_column][\/et_pb_row][\/et_pb_section]<\/p>\n","protected":false},"excerpt":{"rendered":"<p>\u00a0 Blended Wing body research headed by Dr Shabudin bin Mat &nbsp; &nbsp; &nbsp; \u00a0\u00a0\u00a0Experiment on Synthetic jet actuators performance &#8211; Research headed by Dr Nizam Dahalan Coreless Spoiler structure analysis &#8211; Research headed by Dr Haris Ahmad Israr Ahmad and Associate Professor Ainullotfi bin Abdul Latif Helicopter Tail Shake Phenomenon experiment &#8211; Research headed [&hellip;]<\/p>\n","protected":false},"author":11341,"featured_media":0,"comment_status":"open","ping_status":"closed","template":"","meta":{"_et_pb_use_builder":"on","_et_pb_old_content":"<!-- wp:gallery {\"ids\":[5900,5901]} -->\n<figure class=\"wp-block-gallery columns-2 is-cropped\"><ul class=\"blocks-gallery-grid\"><li class=\"blocks-gallery-item\"><figure><img src=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/BWBmodel.jpg\" alt=\"\" data-id=\"5900\" class=\"wp-image-5900\"\/><\/figure><\/li><li class=\"blocks-gallery-item\"><figure><img src=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/BWBmodel2.jpg\" alt=\"\" data-id=\"5901\" data-full-url=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/BWBmodel2.jpg\" data-link=\"https:\/\/research.utm.my\/aerolab\/?attachment_id=5901\" class=\"wp-image-5901\"\/><\/figure><\/li><\/ul><figcaption class=\"blocks-gallery-caption\">Blended Wing body research headed by Dr Shabudin bin Mat<\/figcaption><\/figure>\n<!-- \/wp:gallery -->\n\n<!-- wp:image {\"align\":\"center\",\"id\":5902,\"sizeSlug\":\"large\"} -->\n<div class=\"wp-block-image\"><figure class=\"aligncenter size-large\"><img src=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/synthetic-jet-actuator.png\" alt=\"\" class=\"wp-image-5902\"\/><figcaption>Experiment on Synthetic jet actuators performance - Research headed by Dr Nizam Dahalan<\/figcaption><\/figure><\/div>\n<!-- \/wp:image -->\n\n<!-- wp:gallery {\"ids\":[5905]} -->\n<figure class=\"wp-block-gallery columns-1 is-cropped\"><ul class=\"blocks-gallery-grid\"><li class=\"blocks-gallery-item\"><figure><img src=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/composite2-1024x443.png\" alt=\"\" data-id=\"5905\" data-full-url=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/composite2.png\" data-link=\"https:\/\/research.utm.my\/aerolab\/?attachment_id=5905\" class=\"wp-image-5905\"\/><\/figure><\/li><\/ul><figcaption class=\"blocks-gallery-caption\">Coreless Spoiler structure analysis - Research headed by Dr Haris Ahmad Israr Ahmad<\/figcaption><\/figure>\n<!-- \/wp:gallery -->\n\n<!-- wp:gallery {\"ids\":[5907,5909]} -->\n<figure class=\"wp-block-gallery columns-2 is-cropped\"><ul class=\"blocks-gallery-grid\"><li class=\"blocks-gallery-item\"><figure><img src=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/helicopter-1.jpg\" alt=\"\" data-id=\"5907\" class=\"wp-image-5907\"\/><\/figure><\/li><li class=\"blocks-gallery-item\"><figure><img src=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/helicopter2-1.png\" alt=\"\" data-id=\"5909\" data-full-url=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/helicopter2-1.png\" data-link=\"https:\/\/research.utm.my\/aerolab\/?attachment_id=5909\" class=\"wp-image-5909\"\/><\/figure><\/li><\/ul><figcaption class=\"blocks-gallery-caption\">Helicopter Tail Shake Phenomenon experiment - Research headed by Dr Iskandar Shah Ishak<\/figcaption><\/figure>\n<!-- \/wp:gallery -->\n\n<!-- wp:gallery {\"ids\":[5910,5921]} -->\n<figure class=\"wp-block-gallery columns-2 is-cropped\"><ul class=\"blocks-gallery-grid\"><li class=\"blocks-gallery-item\"><figure><img src=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/CAMAR3.jpg\" alt=\"\" data-id=\"5910\" class=\"wp-image-5910\"\/><figcaption class=\"blocks-gallery-item__caption\">CAMAR III<\/figcaption><\/figure><\/li><li class=\"blocks-gallery-item\"><figure><img src=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/flight-testing-2-1024x536.png\" alt=\"\" data-id=\"5921\" data-full-url=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/flight-testing-2.png\" data-link=\"https:\/\/research.utm.my\/aerolab\/?attachment_id=5921\" class=\"wp-image-5921\"\/><\/figure><\/li><\/ul><figcaption class=\"blocks-gallery-caption\">CAMAR III flight testing - Research Headed by Dr Mohd Nazri, Prof Ir Dr Shuhaimi Mansor<\/figcaption><\/figure>\n<!-- \/wp:gallery -->\n\n<!-- wp:image {\"align\":\"center\",\"id\":5912,\"width\":431,\"height\":384,\"sizeSlug\":\"large\"} -->\n<div class=\"wp-block-image\"><figure class=\"aligncenter size-large is-resized\"><img src=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/CFD1.png\" alt=\"\" class=\"wp-image-5912\" width=\"431\" height=\"384\"\/><figcaption>Vortex induced vibration analysis using CFD - Research headed by Dr Nik Ahmad Ridhwan<\/figcaption><\/figure><\/div>\n<!-- \/wp:image -->\n\n<!-- wp:gallery {\"ids\":[5913,5919]} -->\n<figure class=\"wp-block-gallery columns-2 is-cropped\"><ul class=\"blocks-gallery-grid\"><li class=\"blocks-gallery-item\"><figure><img src=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/propeller-testing-578x1024.jpg\" alt=\"\" data-id=\"5913\" class=\"wp-image-5913\"\/><figcaption class=\"blocks-gallery-item__caption\">Propeller performance testing<\/figcaption><\/figure><\/li><li class=\"blocks-gallery-item\"><figure><img src=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/VTOL-2-1024x373.png\" alt=\"\" data-id=\"5919\" data-full-url=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/VTOL-2.png\" data-link=\"https:\/\/research.utm.my\/aerolab\/?attachment_id=5919\" class=\"wp-image-5919\"\/><figcaption class=\"blocks-gallery-item__caption\">Conceptual VTOL design<\/figcaption><\/figure><\/li><\/ul><figcaption class=\"blocks-gallery-caption\">UAV VTOL design and development. Propeller performance analysis and obstacle avoidance design - Research headed by Dr Mastura Ab Wahid <\/figcaption><\/figure>\n<!-- \/wp:gallery -->\n\n<!-- wp:image {\"id\":5915,\"width\":313,\"height\":232,\"sizeSlug\":\"large\"} -->\n<figure class=\"wp-block-image size-large is-resized\"><img src=\"https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2020\/10\/tedung-kilat.jpg\" alt=\"\" class=\"wp-image-5915\" width=\"313\" height=\"232\"\/><figcaption>Tedung kilat launched in 2010 -research headed by Prof Ir Dr Wan Khairuddin<\/figcaption><\/figure>\n<!-- \/wp:image -->","_et_gb_content_width":"","footnotes":""},"project_category":[],"project_tag":[],"class_list":["post-5899","project","type-project","status-publish","hentry"],"_links":{"self":[{"href":"https:\/\/research.utm.my\/aerolab\/wp-json\/wp\/v2\/project\/5899","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/research.utm.my\/aerolab\/wp-json\/wp\/v2\/project"}],"about":[{"href":"https:\/\/research.utm.my\/aerolab\/wp-json\/wp\/v2\/types\/project"}],"author":[{"embeddable":true,"href":"https:\/\/research.utm.my\/aerolab\/wp-json\/wp\/v2\/users\/11341"}],"replies":[{"embeddable":true,"href":"https:\/\/research.utm.my\/aerolab\/wp-json\/wp\/v2\/comments?post=5899"}],"version-history":[{"count":10,"href":"https:\/\/research.utm.my\/aerolab\/wp-json\/wp\/v2\/project\/5899\/revisions"}],"predecessor-version":[{"id":6286,"href":"https:\/\/research.utm.my\/aerolab\/wp-json\/wp\/v2\/project\/5899\/revisions\/6286"}],"wp:attachment":[{"href":"https:\/\/research.utm.my\/aerolab\/wp-json\/wp\/v2\/media?parent=5899"}],"wp:term":[{"taxonomy":"project_category","embeddable":true,"href":"https:\/\/research.utm.my\/aerolab\/wp-json\/wp\/v2\/project_category?post=5899"},{"taxonomy":"project_tag","embeddable":true,"href":"https:\/\/research.utm.my\/aerolab\/wp-json\/wp\/v2\/project_tag?post=5899"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}