{"id":6784,"date":"2021-08-24T04:51:49","date_gmt":"2021-08-24T04:51:49","guid":{"rendered":"https:\/\/research.utm.my\/aerolab\/?p=6784"},"modified":"2021-08-27T02:10:25","modified_gmt":"2021-08-27T02:10:25","slug":"accepted-papers","status":"publish","type":"post","link":"https:\/\/research.utm.my\/aerolab\/2021\/08\/24\/accepted-papers\/","title":{"rendered":"Accepted Papers"},"content":{"rendered":"

[et_pb_section fb_built=”1″ fullwidth=”on” _builder_version=”4.9.4″ _module_preset=”default”][et_pb_fullwidth_image src=”https:\/\/research.utm.my\/wp-content\/uploads\/sites\/50\/2021\/08\/headerISAE2.png” title_text=”headerISAE2″ _builder_version=”4.9.7″ _module_preset=”default”][\/et_pb_fullwidth_image][\/et_pb_section][et_pb_section fb_built=”1″ custom_padding_last_edited=”off|desktop” admin_label=”hero section” _builder_version=”3.22″ use_background_color_gradient=”on” background_color_gradient_start=”#ffffff” background_color_gradient_end=”#e7edf9″ custom_margin=”|||” custom_padding=”0px||0px|||” custom_padding_tablet=”130px||130px|”][et_pb_row column_structure=”1_2,1_2″ admin_label=”title and illustration” _builder_version=”3.25″ background_size=”initial” background_position=”top_left” background_repeat=”repeat” custom_margin=”|||” custom_padding=”||5px|||”][et_pb_column type=”1_2″ _builder_version=”3.25″ custom_padding=”|||” custom_padding__hover=”|||”][et_pb_text _builder_version=”3.27.4″ text_font=”||||||||” header_font=”Merriweather|700|||||||” header_text_color=”#” header_font_size=”46px” header_line_height=”1.3em” custom_margin=”||0px|” animation_style=”flip” animation_direction=”top”]<\/p>\n

Accepted Papers<\/h1>\n

[\/et_pb_text][et_pb_divider color=”#4646c4″ divider_position=”center” divider_weight=”2px” _builder_version=”3.2″ max_width=”90px” max_width_tablet=”12%” max_width_last_edited=”off|desktop” custom_margin=”|||” animation_style=”flip” animation_delay=”50ms”][\/et_pb_divider][\/et_pb_column][et_pb_column type=”1_2″ _builder_version=”3.25″ custom_padding=”|||” custom_padding__hover=”|||”][\/et_pb_column][\/et_pb_row][\/et_pb_section][et_pb_section fb_built=”1″ _builder_version=”4.9.7″ _module_preset=”default” custom_padding=”57px|||||”][et_pb_row _builder_version=”4.9.7″ _module_preset=”default”][et_pb_column type=”4_4″ _builder_version=”4.9.7″ _module_preset=”default”][et_pb_text _builder_version=”4.9.7″ _module_preset=”default” text_text_color=”#0C71C3″ custom_padding=”23px|||13px||” hover_enabled=”0″ sticky_enabled=”0″]<\/p>\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n
Paper<\/strong> ID<\/strong><\/td>\nTopics<\/strong><\/td>\nList of Authors<\/strong><\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 1<\/strong><\/td>\nBURNING CHARACTERISTIC OF UTM\/AP68AL15HTPB17\/13 PROPELLANT AT 1 ATMOSPHERIC, 2 BAR AND 4 BAR<\/td>\nWan Khairuddin Wan Ali & Muhammad Aiman Talib<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 2<\/strong><\/td>\nEFFECTS OF TRANSITION STRIP ON AERODYNAMIC COEFFICIENTS OF MULDICON WING FOR LOW-SPEED WIND TUNNEL TESTING<\/td>\nBilal Haider, Shuhaimi Mansor, Shabudin Mat, Wan Zaidi Wan Omar, Nazri Nasir<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 3<\/strong><\/td>\nEXPERIMENTAL ANALYSIS FOR LOW-SPEED AERODYNAMIC CHARACTERISTICS OF MULDICON AVT251 UCAV CONFIGURATION<\/td>\nBilal Haider, Shuhaimi Mansor, Shabudin Mat, Wan Zaidi Wan Omar, Nazri Nasir<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 4<\/strong><\/td>\nCHARACTERIZATION OF UNSTEADY AERODYNAMIC WAKE FOR A GENERIC HELICOPTER<\/td>\nNur Nabilla Mohd, Iskandar Shah Ishak, Shabudin Mat, and Airi Ali<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 5<\/strong><\/td>\nSPECTROSCOPIC ANALYSIS OF SOYBEAN BIODIESEL SWIRL FLAME<\/td>\nMeng-Choung Chiong & Guo Ren Mong<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 6<\/strong><\/td>\nPERFORMANCE OF A BLENDED WING-BODY VTOL UNMANNED AERIAL VEHICLE FOR MEDICAL TRANSPORT APPLICATION<\/td>\nNur S. M. Ikhwan, Rizal E. M. Nasir, W. Mazlina W. Mohamed, Iskandar S. Ishak & Wahyu Kuntjoro<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 7<\/strong><\/td>\nROTATIONAL SPEED ANALYSIS ON DOUBLE ROTATING CYLINDER FOR CYFLAP USING NUMERICAL METHOD<\/td>\nMuhammad Syakir Iman Roslan, Hidayatullah Mohammad Ali & Azmin Shakrine Mohd Rafie<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 8<\/strong><\/td>\nEXPERIMENTAL AND NUMERICAL STUDY ON THE VORTICAL FLOW OF MULDICON CONFIGURATION<\/td>\nIbrahim Madan, Jiun-Jih Miau & Shabudin Bin Mat<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 9<\/strong><\/td>\nINVESTIGATION OF SYMMETRIC CROSS-PLY AND ANGLE-PLY LAMINATE DUE TO STATIC AERODYNAMIC LOAD ON HIGH ASPECT RATIO COMPOSITE WING<\/td>\nMatza Gusto Andika, Ilham Akbar Adi Satriya, and Fadilah Hasim<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 10<\/strong><\/td>\nA CFD ANALYSIS OF WINDOW-TO-WALL RATIO AND OPENING SIZE ON NATURAL VENTILATION AND THERMAL COMFORT OF AN ECO-HOUSE<\/td>\nIhab Jabbar Al Rikabi, Mohamed Ali Abuelnour, Adil A. M. Omara, Najib Aminu Ismail, Farid Nasir Ani, Shabudin Bin Mat<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 11<\/strong><\/td>\nDEVELOPMENT AND FLIGHT STABILITY TEST OF AN AMBULANCE UAV<\/td>\nWan Mazlina Wan Mohamed, Nur Fahimah Mat Salleh, Rizal Effendy Mohd Nasir, Siti Mariam Abdul Rahman, Shafiq Suhaimi<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 12<\/strong><\/td>\nSIMULATION STUDY ON THE PERFORMANCE OF OTEC USING DIFFERENT WORKING FLUID<\/td>\nMuhammad Ajwad Bin Wahinuddin, Dr. -ing. Mohd Nazri Bin Mohd Nasir, Norazila Othman, Shabudin Bin Mat<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 13<\/strong><\/td>\nDIVERSIFYING AEROLAB RESOURCES FOR INCOME GENERATION<\/td>\nWan Khairuddin Wan Ali<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 14<\/strong><\/td>\nSTRUCTURAL ANALYSIS OF RADIAL TURBINE IMPELLER FOR OTEC<\/td>\nI.Z. Suhaini, A. Abdul-Latif\u00a0 & Shamsudin. M.F.<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 15<\/strong><\/td>\nTHE INFLUENCE OF SEAT PITCH AND BODY ANTHROPOMETRY PARAMETERS ON AIRCRAFT PASSENGERS\u2019 SEATING COMFORT<\/td>\nNadia Hanani Ahmad Habibillah, Nur Hidayah Ismail, Fairuz Izzuddin Romli, and Ezanee Gires<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 16<\/strong><\/td>\nPERFORMANCE ANALYSIS OF A YELLOW OLEANDER SEED OIL BIODIESEL POWERED AERO DERIVATIVE GAS TURBINE ENGINE<\/td>\nA. A. Linus , M. U. Bonnet, W. C. Solomon, M. U. Kaisan, B. G. Ibrahim and N. A. Ismail<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 17<\/strong><\/td>\nCONTINUOUS WAVELET TRANSFORM FOR VIBRATIONAL NOISE ANALYSIS OF MANUAL DRILLING PROCESS<\/td>\nMohd Firdaus Shamsuddin, Muhammad Hanafi Azami, Hasan Firdaus Mohd Zaki and Nur Azam Abdullah<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 18<\/strong><\/td>\nAMPLITUDE MODULATION OF A QUASI-UNIMODAL CAVITY TONE IN A LOW-SPEED FLOW<\/td>\nVarun Thangamani<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 19<\/strong><\/td>\nOPTIMISATION OF THE COMBUSTION PERFORMANCE WHEN FIRING WASTE COOKING OIL BIODIESEL BLENDS IN A LIQUID FUEL BURNER<\/td>\nMuhammad Syahiran Abdul Malik, Mohammad Nazri Mohd Jaafar, Norazila Othman, Mohd Shuisma Mohd Ismail, Muhammad Roslan Rahim & Mazlan Said<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 20<\/strong><\/td>\nIMPACT OF SOLIDITY ON AERODYNAMIC PERFORMANCE OF VERTICAL AXIS WIND TURBINE<\/td>\nKok Hoe Wong, Shern Khai Ung, Yong Hua Tang, Jo Han Ng, and Wen Tong Chong<\/td>\n<\/td>\n<\/tr>\n
ISAE PAER 21<\/strong><\/td>\nADHESION DURABILITY OF METAL\/EPOXY ADHESIVELY BONDED UNDER TROPICAL WEATHERING EXPOSURE<\/td>\nNor Ashiqeen Jamaluddin, Muhammad Airul Amin Md Dani, Mahzan Johar, and Shukur Abu Hassan<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 22<\/strong><\/td>\nAERODYNAMIC CHARACTERISTICS OF NACA0012 WITH SUCTION AND BLOWING SLOTS AT VARIOUS ANGLES OF ATTACK<\/td>\nAhmad Hussein Abdul Hamid, Muhammad Azuan Mohd Najib, Rizal Effendy Mohd Nasir<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 23<\/strong><\/td>\nCFD ANALYSIS OF ROCKET CONVERGENT-DIVERGENT NOZZLE WITH SWIRL VANES FOR IMPROVED STABILITY<\/td>\nAhmad Hussein bin Abdul Hamid, Akma Noor Asyikin binti Omar, Zuraidah Salleh, Mohammad Juani Sujana ,\u00a0 Mohamad Amirul Muhammad, Mohd Shahar Saad, Mohd Ismail Khamis<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 24<\/strong><\/td>\nMICRO VORTEX GENERATOR IN IMPROVING AERODYNAMIC PERFORMANCE OF WIG AIRCRAFT<\/td>\nZinnyrah M, Syahin AAT, Sulaiman MS, Che Idris A, Rahman MRA and Saad MR<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 25<\/strong><\/td>\nREDUCING THE FUEL CONSUMPTION BY USING VARIABLE STABILITY TECHNIQUE<\/td>\nYaseer Abdallha Mahjob, Ola Mohamed Taha and Monzer KamalAlden Ismail<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 26<\/strong><\/td>\nA COMPARATIVE EXPERIMENTAL STUDY ON THE MIXING CHARACTERISTICS OF TWO DIFFERENT TWIN JETS<\/td>\nA.Muthuram and S.Thanigaiarasu<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 27<\/strong><\/td>\nPRELIMINARY STRUCTURAL DESIGN OF CORELESS SPOILER BY TOPOLOGICAL OPTIMIZATION<\/td>\nH.A Israr, T.S Chwen, A.A Latif, K.J Wong<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 28<\/strong><\/td>\nNUMERICAL ANALYSES FOR REGRESSION RATE SOLID FUEL DOPED WITH HIGH ENTROPY ALLOYS IN HYBRID ROCKET MOTOR<\/td>\nSiti Nurfaiqah binti Asmuni, Izham izzat ismail, Muhammad Hanafi Azami1, Nur Azam Abdullah & Norhuda Hidayah Nordin<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 29<\/strong><\/td>\nASSESSMENT ON AERODYNAMIC TESTING OF A CIVIL AIRCRAFT IN INDONESIA LOW-SPEED WIND TUNNEL (ILST) USING ANALYSIS OF VARIANCE<\/td>\nSubagyo Subagyo<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 30<\/strong><\/td>\nEFFECTS OF COMPOSITE LAMINATES TOWARDS FLUTTER SPEED<\/td>\nNurul-Zubaidah Zaki, Afiqah Nizar, Shuhaimi Mansor and Ainullotfi Abdul-Latif<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 31<\/strong><\/td>\nSTRUCTURAL DAMPING MODEL FOR FLUTTER ANALYSIS OF COMPOSITE WING<\/td>\nNurul-Zubaidah Zaki, Zuha Fathullah, Shuhaimi Mansor, and Ainullotfi Abdul-Latif<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 32<\/strong><\/td>\nDESIGN AND IMPLEMENTATION OF PBS CANSAT FOR MALAYSIA SISWASAT 2020 COMPETITION<\/td>\nNorisza Dalila Binti Ismail , Mohamad Khairani Bin Mohamed Amin, Nurul Farhana Binti Mohd Faizul, Nur Eliana Binti Md Zahirul Islam, Nur Aricesa Hairani Binti Hairuddin, Putera Danish Daniaal Bin Jaffry and Joanis Anak Enteri<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 33<\/strong><\/td>\nPERFORMANCE AND EMISSION ANALYSIS OF NEEM OIL BIO-DIESEL WITH PENTANOL BLEND IN DIESEL ENGINE<\/td>\nAdamu Sulaiman, Umar Ali Umar, Muhammad Usman Kaisan, Ibrahim Umar Ibrahim, Shitu Abubakar, and Oyedeji Ayodeji Nathaniel.<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 34<\/strong><\/td>\nEFFECT OF PRESSURE DISTRIBUTION OF NREL S809 AIRFOIL WITH RECTANGULAR VORTEX GENERATOR<\/td>\nBalaji G, Muthuram A, Madhan Raj V<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 35<\/strong><\/td>\nCOMPUTATIONAL FLUID DYNAMIC (CFD) ANALYSIS ON PERFORMANCE OF A ROTATING PROPELLER<\/td>\nLeong Chee Hang, Mastura Ab Wahid, Nik Ahmad Ridhwan Nik Mohd, Norazila Othman & Mohd Zarhamdy Md. Zain<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 36<\/strong><\/td>\nDISTANCE BASED CALCULATION FOR AIRPORT RUNWAY CAPACITY<\/td>\nNurul Amirah Binti Muhamad, S.M.B. Abdul Rahman, Wan Mazlina Wan Mohamed<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 37<\/strong><\/td>\nNUMERICAL ANALYSIS ON THE EFFECT OF LONGITUDINAL PLACEMENT OF VORTEX GENERATORS FOR JET CONTROL<\/td>\nBalamani G & Thanigaiarasu S<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 38<\/strong><\/td>\nTHERMODYNAMIC ANALYSIS ON A NEW REVISED OTEC CYCLE USING AMMONIA<\/td>\nMuhammad Aiman Wafi\u00a0 Suruji, Nazri Nasi, Norazila Othman, Wan Zaidi Wan Omar, Shabudin Mat<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 39<\/strong><\/td>\nEFFECT OF FLOW COEFFICIENT AND ROTOR RADIUS RATIO ON RADIAL TURBINE ANALYSIS<\/td>\nA. R. Jasmi, S. Mansor, N. Othman, M. Ab Wahid,\u00a0 N.A.R. Nik Mohd, N. Nasir, M. N. Dahalan,<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 40<\/strong><\/td>\nPRELIMINARY STUDIES USING NUMERICAL ANALYSIS OF THE AERODYNAMIC LIFT AND DRAG OVER SACCON UCAV<\/td>\nNormeelaiva Al-hussien, Nur Amalina Musa & Muhammad Ahmar Zuber<\/td>\n<\/td>\n<\/tr>\n
<\/td>\n<\/tr>\n
ISAE PAPER 41<\/strong><\/td>\nDEVELOPMENT OF AUTOMATED WAREHOUSE INVENTORY MANAGEMENT SYSTEM USING DRONE TECHNOLOGY AND RFID SYSTEM<\/td>\nMahmoud Gamal Fathalla, Nazri Nasir, Ruzairi Abdul Rahim, Abu Sahmah Supa\u2019at, Mohd Adib Sarijari and Sophan Wahyudi Nawawi<\/td>\n<\/td>\n<\/tr>\n
ISAE PAPER 42<\/strong><\/td>\nPRELIMINARY ANALYSIS OF A SHOOTER STABILIZATION SYSTEM FOR MULTI-ROTOR DRONE WEAPON SYSTEM<\/td>\nMuhammad Husainii Zulkifly\u00a0 & \u00a0Abd. Rahim Abu Talib<\/td>\n<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n

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Accepted Papers Paper ID Topics List of Authors ISAE PAPER 1 BURNING CHARACTERISTIC OF UTM\/AP68AL15HTPB17\/13 PROPELLANT AT 1 ATMOSPHERIC, 2 BAR AND 4 BAR Wan Khairuddin Wan Ali & Muhammad Aiman Talib ISAE PAPER 2 EFFECTS OF TRANSITION STRIP ON AERODYNAMIC COEFFICIENTS OF MULDICON WING FOR LOW-SPEED WIND TUNNEL TESTING Bilal Haider, Shuhaimi Mansor, Shabudin […]<\/p>\n","protected":false},"author":11341,"featured_media":0,"comment_status":"closed","ping_status":"closed","sticky":false,"template":"elementor_header_footer","format":"standard","meta":{"_et_pb_use_builder":"on","_et_pb_old_content":"","_et_gb_content_width":"1080","footnotes":""},"categories":[4],"tags":[],"class_list":["post-6784","post","type-post","status-publish","format-standard","hentry","category-isae2021"],"_links":{"self":[{"href":"https:\/\/research.utm.my\/aerolab\/wp-json\/wp\/v2\/posts\/6784","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/research.utm.my\/aerolab\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/research.utm.my\/aerolab\/wp-json\/wp\/v2\/types\/post"}],"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=6784"}],"version-history":[{"count":5,"href":"https:\/\/research.utm.my\/aerolab\/wp-json\/wp\/v2\/posts\/6784\/revisions"}],"predecessor-version":[{"id":6914,"href":"https:\/\/research.utm.my\/aerolab\/wp-json\/wp\/v2\/posts\/6784\/revisions\/6914"}],"wp:attachment":[{"href":"https:\/\/research.utm.my\/aerolab\/wp-json\/wp\/v2\/media?parent=6784"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/research.utm.my\/aerolab\/wp-json\/wp\/v2\/categories?post=6784"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/research.utm.my\/aerolab\/wp-json\/wp\/v2\/tags?post=6784"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}