Zobrazeno 1 - 10
of 30
pro vyhledávání: '"Rizal Effendy Mohd Nasir"'
Autor:
null Fairuz Izzuddin Romli, null Muhammad Aiman Mohammad Sabri, null Rizal Effendy Mohd Nasir
Publikováno v:
CFD Letters. 15:12-21
Although unmanned aerial vehicle (UAV) has found many applications in various fields, its operation has been constrained by its low flight endurance. To date, several design efforts are pursued to improve this performance and one of them is the explo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0a13a533ab958666a527bb3aa2b934c2
https://doi.org/10.37934/cfdl.15.3.1221
https://doi.org/10.37934/cfdl.15.3.1221
Publikováno v:
JOURNAL OF APPLIED ENGINEERING DESIGN AND SIMULATION. 2:1-10
Lap joints are commonly used as a method of connecting structural parts. This includes parts that are made by 3D printing technology. Structural simulation using the finite element (FE) method can be used for lap joint analysis purposes. There are tw
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::971b715982fb9ae60490e19412ab5994
https://doi.org/10.24191/jaeds.v2i2.43
https://doi.org/10.24191/jaeds.v2i2.43
Publikováno v:
2020 IEEE 8th Conference on Systems, Process and Control (ICSPC).
Quadcopters are multirotor drones equipped with four rotors where hovering, banking, forward and backward motions can be controlled by the thrust produced by the propellers. This paper describes simulation of the quadcopter dynamics through thrust di
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::da5c12b1861b8c779feb077a79e4144a
https://doi.org/10.1109/icspc50992.2020.9305799
https://doi.org/10.1109/icspc50992.2020.9305799
Publikováno v:
2019 IEEE 7th Conference on Systems, Process and Control (ICSPC).
Quadcopter is a multirotor-drone that consists of four motors. The thrust produced by motors is adjustable to give command to the quadcopter such as hovering, forward and backward motions, roll, yaw and pitch. Varying the thrust of motor affects the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7112e77e9604983f8294a15974b7c298
https://doi.org/10.1109/icspc47137.2019.9068094
https://doi.org/10.1109/icspc47137.2019.9068094
Autor:
Zurriati Mohd Ali, Wirachman Wisnoe, Ehan Sabah Shukri Askari, Nornashiha Mohd Saad, Rizal Effendy Mohd Nasir
Publikováno v:
MATEC Web of Conferences, Vol 256, p 02004 (2019)
This paper presents an aerodynamic characteristic study in longitudinal direction of UiTM Blended Wing Body-Unmanned Aerial Vehicle Prototype (BWB-UAV Prototype) equipped with horizontal stabilizers. Flight tests have been conducted and as the result
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b1d7297f19fa2b7f53907ab5d3a51c6e
https://doaj.org/article/77c3bc74081e43c0b511450962018cf5
https://doaj.org/article/77c3bc74081e43c0b511450962018cf5
Publikováno v:
Procedia Technology. 15:783-791
Blended wing-body (BWB) concept promises up to 30 percent increase in aerodynamic efficiency and reduction in fuel cost by having planform geometry optimized to increase lift and to reduce drag. Many claimed to have achieved the target of increasing
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a5607d9757a0dba3c8c76990406b8bac
https://doi.org/10.1016/j.protcy.2014.09.051
https://doi.org/10.1016/j.protcy.2014.09.051
Autor:
Norhisyam Jenal, Firdaus Mohamad, Wirachman Wisnoe, Khairul Imran Sainan, Rizal Effendy Mohd Nasir
Publikováno v:
Applied Mechanics and Materials. 393:323-328
This paper presents a study about yaw stability analysis for UiTMs Blended-Wing-Body (BWB) Baseline-II E-4. This aircraft is equipped with split drag flaps in order to perform directional motion. One of the split drag flaps will be deflected to gener
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::13f9635e855af6a9202f173b04470a1a
https://doi.org/10.4028/www.scientific.net/amm.393.323
https://doi.org/10.4028/www.scientific.net/amm.393.323
Publikováno v:
Applied Mechanics and Materials. 393:329-337
Transient response of an aircraft in longitudinal motion has two modes of oscillatory motion short period mode and phugoid modes and failure to achieve satisfactory level would mean poor flying and handling qualities leading to unnecessary pilot work
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6e6e01a30e323a215fdeba3cd19ae82e
https://doi.org/10.4028/www.scientific.net/amm.393.329
https://doi.org/10.4028/www.scientific.net/amm.393.329
Publikováno v:
Applied Mechanics and Materials. 225:375-384
Phugoid mode is a lowly damped, low-frequency oscillatory motion representing vertical translation usually related to kinetic and potential energy interchange. MIL-F-8785C standard has ruled out qualitative specification requirements on measurement o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::03925725e328f794037d18fff4fffc71
https://doi.org/10.4028/www.scientific.net/amm.225.375
https://doi.org/10.4028/www.scientific.net/amm.225.375
Autor:
Ramlan Kasiran, Mohd Faizal Mohamad, Amir Radzi Ab. Ghani, Rizal Effendy Mohd Nasir, Wan Ahmad Najmi Wan Mohamed, Mohd Shahriman Adenan, Mohd Haniff Mat
Publikováno v:
Applied Mechanics and Materials. 165:237-241
Thin-walled metallic tubular structures are generally used as impact energy absorber in automotive structures due to their ease of fabrication and installation, high energy absorption capacity and long stroke. However, unlike a normal passenger car w
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9931b3510d0187beeee09d22b87f3e42
https://doi.org/10.4028/www.scientific.net/amm.165.237
https://doi.org/10.4028/www.scientific.net/amm.165.237