Performance Analysis Of A Compliant Wing For A Light Aircraft
Main purpose of this project is to apply the compliant mechanism into aircraft wing. It can improve the flight performance of conventional light aircraft. A compliant mechanism is flexible structure that elastically deforms without joints to produce a desired force or displacement. This study...
| Main Author: | Mohamad Sidik, Mohamad Sabri |
|---|---|
| Format: | Monograph |
| Language: | English |
| Published: |
Universiti Sains Malaysia
2005
|
| Subjects: | |
| Online Access: | http://eprints.usm.my/58203/ http://eprints.usm.my/58203/1/Performance%20Analysis%20Of%20A%20Compliant%20Wing%20For%20A%20Light%20Aircraft_Mohamad%20Sabri%20Mohamad%20Sidik.pdf |
Similar Items
Drag analysis of an aircraft wing model and without bird feather like winglet
by: Hossain, Altab, et al.
Published: (2012)
by: Hossain, Altab, et al.
Published: (2012)
Estimation of Aerodynamic Characteristics of a Light Aircraft
by: Ishak, Iskandar Shah, et al.
Published: (2006)
by: Ishak, Iskandar Shah, et al.
Published: (2006)
Further Evaluation Of Aerodynamic Characteristics Of The Aero 3 Trainer Aircraft Wing
by: Thirunavakarasu, Prakash
Published: (2000)
by: Thirunavakarasu, Prakash
Published: (2000)
Fundamental study of hybrid graphene oxide and nanofibrillated cellulose for aircraft wings application
by: Kumaran, Kadirgama, et al.
by: Kumaran, Kadirgama, et al.
Real-time Monitoring System of Composite Aircraft Wings Utilizing Fibre Bragg Grating Sensor
by: Vorathin, E., et al.
Published: (2016)
by: Vorathin, E., et al.
Published: (2016)
The analysis of wing performance for reconnaissance UAV
by: Zulkifli, Yusof
Published: (2009)
by: Zulkifli, Yusof
Published: (2009)
Development of educational software for stress analysis of an aircraft wing
by: Mohamed Ali, Jaafar Syed, et al.
Published: (2012)
by: Mohamed Ali, Jaafar Syed, et al.
Published: (2012)
Modelling and structural analysis of three-dimensional wing
by: Mohd Zakuan, Muhammad Amir Mirza, et al.
Published: (2019)
by: Mohd Zakuan, Muhammad Amir Mirza, et al.
Published: (2019)
Nonlinear modeling of compliant mechanism
by: Khan, Md. Raisuddin, et al.
Published: (2013)
by: Khan, Md. Raisuddin, et al.
Published: (2013)
Reverse engineering of micro light aircraft systems and design
by: Wan Hassan, Wan Azizurrahman
Published: (2014)
by: Wan Hassan, Wan Azizurrahman
Published: (2014)
Identification of Nonlinearities in Joints of a Wing Structure
by: M. S. M., Sani, et al.
Published: (2016)
by: M. S. M., Sani, et al.
Published: (2016)
A synthesis of an aircraft approach, landing & overrun
by: Perumal, Kannan, et al.
Published: (2008)
by: Perumal, Kannan, et al.
Published: (2008)
Analysis of one way valve mechanism for wings of a flapping drone / Deng Xinchen
by: Deng, Xinchen
Published: (2020)
by: Deng, Xinchen
Published: (2020)
Design of flapping mechanism and analysis on the lift force of the wings / Saktishvikmend Anbalagan
by: Saktishvikmend, Anbalagan
Published: (2019)
by: Saktishvikmend, Anbalagan
Published: (2019)
Aerodynamic behavior of a compound wing configuration in ground effect
by: Jamei, Saeed, et al.
Published: (2014)
by: Jamei, Saeed, et al.
Published: (2014)
Fluid-Structure Interaction Analysis On Aircraft Wing Intergrated With Wing Tip Device
by: Tan, Yao Bin
Published: (2021)
by: Tan, Yao Bin
Published: (2021)
Gust load alleviation of flexible composite wing
by: Ibren, Mohamed, et al.
Published: (2020)
by: Ibren, Mohamed, et al.
Published: (2020)
Experimental Study On The Wing Structure And Skin Flexibility For Flapping Wing Of Micro Aerial Vehicle (MAV)
by: Rashid, Rohayati Ab
Published: (2011)
by: Rashid, Rohayati Ab
Published: (2011)
Methods of aircraft trajectory optimisation in air combat
by: Nusyirwan, Istas Fahrurrazi, et al.
Published: (2007)
by: Nusyirwan, Istas Fahrurrazi, et al.
Published: (2007)
Comprehensive analysis of a light weight lift system
by: Mohd Fauzi, Muhammad
Published: (2010)
by: Mohd Fauzi, Muhammad
Published: (2010)
Experimental Study on the Effect of Skin Flexibility on Aerodynamic Performance of Flapping Wings for Micro Air Vehicles
by: Hamid, Yusoff, et al.
Published: (2014)
by: Hamid, Yusoff, et al.
Published: (2014)
Experimental investigation of plain- and flapped-wing tip vortices
by: Elsayed, Omer Ali, et al.
Published: (2009)
by: Elsayed, Omer Ali, et al.
Published: (2009)
Model and control on the ascending process of rotating wing helicopter
by: Noor Zalika, Kornain
Published: (2013)
by: Noor Zalika, Kornain
Published: (2013)
Structural Analysis Of Thermoformed Electroluminescent Printed Lighting
by: Chiang, Han Xi
Published: (2019)
by: Chiang, Han Xi
Published: (2019)
Fuzzy logic approach for estimation of longitudinal aircraft parameters
by: Yaacob, M. S., et al.
Published: (2002)
by: Yaacob, M. S., et al.
Published: (2002)
Fuzzy logic approach for prediction the lift coefficient on an aircraft model with and without winglet
by: Hossain, Altab, et al.
Published: (2009)
by: Hossain, Altab, et al.
Published: (2009)
Application of fuzzy logic approach for an aircraft model with and without winglet
by: Hossain, Altab, et al.
Published: (2011)
by: Hossain, Altab, et al.
Published: (2011)
Wing design for blended-wing-body aircraft
by: Mat Yazik, Muhamad Hasfanizam, et al.
Published: (2017)
by: Mat Yazik, Muhamad Hasfanizam, et al.
Published: (2017)
Effects of different water percentages in non-surfactant emulsion fuel on performance and exhaust emissions of a light-duty truck
by: Nurul Aiyshah, Mazlan, et al.
Published: (2018)
by: Nurul Aiyshah, Mazlan, et al.
Published: (2018)
The design of reusable endosurgical grasper using compliant mechanism / Solehuddin Shuib...[et al.]
by: Shuib*,, Solehuddin, et al.
Published: (2019)
by: Shuib*,, Solehuddin, et al.
Published: (2019)
Witness Simulation Of Machine Breakdowns For Small, Medium And Large Aircrafts During Turnaround Process
by: Hashim, Nur Amanina Ayuni
Published: (2022)
by: Hashim, Nur Amanina Ayuni
Published: (2022)
Stress And Aeroelastic Analyses Of Ultralight Aircraft Wing
by: Kabbarah, Hussam Fatthi A
Published: (2021)
by: Kabbarah, Hussam Fatthi A
Published: (2021)
Design and development of cross flow delta-wing water turbine for Pahang river
by: Mohd Izzat, Kamarulzaman
Published: (2012)
by: Mohd Izzat, Kamarulzaman
Published: (2012)
Fabrication and testing of IIUM aircraft fuselage structure made of composite laminate material
by: Aminanda, Yulfian, et al.
Published: (2011)
by: Aminanda, Yulfian, et al.
Published: (2011)
Finite element model updating of riveted joints of simplified model aircraft structure
by: M. A., Yunus, et al.
Published: (2018)
by: M. A., Yunus, et al.
Published: (2018)
Design and development of noise detector at hangar aircraft training organisation / Norsiah Sukardy
by: Norsiah , Sukardy
Published: (2018)
by: Norsiah , Sukardy
Published: (2018)
The design of a high aspect ratio HALE aircraft composite wing. part I: static strength analysis / Bambang K. Hadi, Muhammad A. Ghofur and IndraPermana
by: Hadi, Bambang K., et al.
Published: (2015)
by: Hadi, Bambang K., et al.
Published: (2015)
Experimental And Numerical Investigations On The Performance Of Flexible Skin Flapping Wing For Micro Aerial Vehicle Application
by: Yusoff, Hamid
Published: (2013)
by: Yusoff, Hamid
Published: (2013)
Design and analysis light weight lift system for disable people
by: Siti Fatimah, Ismail
Published: (2008)
by: Siti Fatimah, Ismail
Published: (2008)
The development of a fixed wing aircraft analysis and design flight dynamic software
by: Ahmad Alaian, Ahmad Eshtiwey
Published: (2016)
by: Ahmad Alaian, Ahmad Eshtiwey
Published: (2016)
Similar Items
-
Drag analysis of an aircraft wing model and without bird feather like winglet
by: Hossain, Altab, et al.
Published: (2012) -
Estimation of Aerodynamic Characteristics of a Light Aircraft
by: Ishak, Iskandar Shah, et al.
Published: (2006) -
Further Evaluation Of Aerodynamic Characteristics Of The Aero 3 Trainer Aircraft Wing
by: Thirunavakarasu, Prakash
Published: (2000) -
Fundamental study of hybrid graphene oxide and nanofibrillated cellulose for aircraft wings application
by: Kumaran, Kadirgama, et al. -
Real-time Monitoring System of Composite Aircraft Wings Utilizing Fibre Bragg Grating Sensor
by: Vorathin, E., et al.
Published: (2016)