A matlab based educational software for the study on the effect of cut-out in aircraft wings
Cut-outs on aircraft wings are unavoidable due to the placement of fuel tanks and retraction of landing gear inside the wing. The stresses acting on an aircraft wing will deviate substantially before and after a cut-out is made and therefore it is crucial to perform stress analysis in an aircraft wi...
| Main Authors: | Mohammed Riyadh, Miah, Syed Mohamed Ali, Jaffar |
|---|---|
| Format: | Article |
| Language: | English English |
| Published: |
Science Publishing Corporation Inc
2018
|
| Subjects: | |
| Online Access: | http://irep.iium.edu.my/68441/ http://irep.iium.edu.my/68441/1/68441_A%20Matlab%20Based%20Educational%20Software.pdf http://irep.iium.edu.my/68441/2/68441_A%20Matlab%20Based%20Educational%20Software_SCOPUS.pdf |
Similar Items
Educational software for stress analysis of non-idealized closed thin-walled sections
by: Syed Mohamed Ali, Jaffar, et al.
Published: (2018)
by: Syed Mohamed Ali, Jaffar, et al.
Published: (2018)
Educational software for stress analysis of idealized closed thin walled sections
by: Syed Mohamed Ali, Jaffar, et al.
Published: (2018)
by: Syed Mohamed Ali, Jaffar, et al.
Published: (2018)
Aeroelastic passive control optimization of supersonic composite wing with external stores
by: Sulaeman, Erwin, et al.
Published: (2017)
by: Sulaeman, Erwin, et al.
Published: (2017)
Software development for aerodynamic characteristics estimation of wing-body combination of aircraft at cubsonic speeds
by: Dahalan, Md. Nizam, et al.
Published: (2001)
by: Dahalan, Md. Nizam, et al.
Published: (2001)
Design of IIUM aircraft fuselage using composite material
by: Aminanda, Yulfian, et al.
Published: (2011)
by: Aminanda, Yulfian, et al.
Published: (2011)
Fluid-structure interactions of variable span wings in low Reynold flows
by: Salleh, Hafiz, et al.
Published: (2018)
by: Salleh, Hafiz, et al.
Published: (2018)
The aerodynamics analysis of type UAV aircraft with pusher engine configuration by use of DATCOM software
by: Al Aian, Ahmad Eshtiwey
Published: (2011)
by: Al Aian, Ahmad Eshtiwey
Published: (2011)
Effects of bio-inspired surface roughness on a swept back tapered NACA 4412 wing
by: Malik, Khurshid, et al.
Published: (2019)
by: Malik, Khurshid, et al.
Published: (2019)
Spring-back of thick uni-directional carbon fibre reinforced composite laminate for aircraft structure application
by: Zakaria, Mohd Hafizu, et al.
Published: (2018)
by: Zakaria, Mohd Hafizu, et al.
Published: (2018)
Educational software for stress analysis of an aircraft fuselage
by: Mohamed Ali, Jaafar Syed, et al.
Published: (2010)
by: Mohamed Ali, Jaafar Syed, et al.
Published: (2010)
The flight trajectory analysis on the existing aircraft
by: M Khalifa, Tarek M.
Published: (2012)
by: M Khalifa, Tarek M.
Published: (2012)
On the development of computer code for aircraft flight dynamics analysis
by: Mohamed Alazomui, Outman
Published: (2014)
by: Mohamed Alazomui, Outman
Published: (2014)
Educational software for stress analysis of non-idealized closed thin-walled sections
by: Mohamed Ali, Jaffar Syed, et al.
Published: (2019)
by: Mohamed Ali, Jaffar Syed, et al.
Published: (2019)
Literature review : Biomimetic and conventional aircraft wing tips
by: Ahmed Siddiqui, Naseeb, et al.
Published: (2017)
by: Ahmed Siddiqui, Naseeb, et al.
Published: (2017)
Evaluation of aircraft wing-tip vortex using PIV
by: Elsayed, Omer Ali, et al.
Published: (2009)
by: Elsayed, Omer Ali, et al.
Published: (2009)
Aerofracturelastic on wing box of multi-purpose commuter aircraft under gust lby means of XFEM
by: Abdullah, Nur Azam, et al.
Published: (2018)
by: Abdullah, Nur Azam, et al.
Published: (2018)
ESA 343/2 AIRCRAFT AERODYNAMICS [AERODINAMIK PESAWAT] (DECEMBER 2016 / JANUARY 2017)
by: PPKA, Pusat Pengajian Kejuruteraan Aeroangkasa
Published: (2017)
by: PPKA, Pusat Pengajian Kejuruteraan Aeroangkasa
Published: (2017)
ESA 343/2 AIRCRAFT AERODYNAMICS [AERODINAMIK PESAWAT] (DECEMBER 2015 / JANUARY 2016)
by: PPKA, Pusat Pengajian Kejuruteraan Aeroangkasa
Published: (2016)
by: PPKA, Pusat Pengajian Kejuruteraan Aeroangkasa
Published: (2016)
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)
Experimental and numerical study on the aerodynamics and stability characteristics of a canard aircraft
by: Syed Mohamed Ali, Jaffar, et al.
Published: (2019)
by: Syed Mohamed Ali, Jaffar, et al.
Published: (2019)
Effect of wing loading on gross takeoff mass of a hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2016)
by: UlHaque, Anwar, et al.
Published: (2016)
Hydrostatic and hydrodynamic characteristics of swimming animals: an inspiration for hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2015)
by: UlHaque, Anwar, et al.
Published: (2015)
Analysis on cracked commuter aircraft wing under dynamic cruise load by means of XFEM
by: Wirawan, Nanda, et al.
Published: (2018)
by: Wirawan, Nanda, et al.
Published: (2018)
Hybrid buoyant aircraft: future STOL aircraft for interconnectivity of the Malaysian islands
by: UlHaque, Anwar, et al.
Published: (2017)
by: UlHaque, Anwar, et al.
Published: (2017)
Crash analysis of an aircraft fuselage under belly landing
by: Syed Mohamed Ali, Jaffar, et al.
Published: (2017)
by: Syed Mohamed Ali, Jaffar, et al.
Published: (2017)
Experimental investigation of the base flow from the nozzles with sudden expansion
by: Chaudhary, Zakir Ilahi, et al.
Published: (2015)
by: Chaudhary, Zakir Ilahi, et al.
Published: (2015)
Effect of area ratio on base pressure in a suddenly expanded duct for under expanded flow ft mach 1.87
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)
Control of nozzle flow in a suddenly expanded duct with micro jets
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)
Effect of mach number in a suddenly expanded flow for area ratio 4.84
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)
Study of feasibility of pulse detonation engine powered by alternative fuels
by: Warimani, Mohammad Salman, et al.
Published: (2019)
by: Warimani, Mohammad Salman, et al.
Published: (2019)
Comparison of black-grey-white box approach in system identification of a flight vehicle
by: Nugroho, Larasmoyo, et al.
Published: (2018)
by: Nugroho, Larasmoyo, et al.
Published: (2018)
A Model Predictive Control (MPC) approach on unit quaternion orientation based quadrotor for trajectory tracking
by: Maidul, Isla, et al.
Published: (2019)
by: Maidul, Isla, et al.
Published: (2019)
Effects of micro jets on the flow field of the duct with sudden expansion
by: Akhtar, Mohammad Nishat, et al.
Published: (2019)
by: Akhtar, Mohammad Nishat, et al.
Published: (2019)
Autonomous control of tilt tri-rotor unmanned aerial vehicle
by: Olanrewaju, Rashidah Funke, et al.
Published: (2016)
by: Olanrewaju, Rashidah Funke, et al.
Published: (2016)
Experimental study of the strength of sandwich structure with honeycomb core
by: Aminanda, Yulfian, et al.
Published: (2011)
by: Aminanda, Yulfian, et al.
Published: (2011)
Advances in Aircraft Structures
Published: (2011)
Published: (2011)
Flow visualization over a circular planform wing
by: Suliman , M. M. Ali, et al.
Published: (2013)
by: Suliman , M. M. Ali, et al.
Published: (2013)
Educational software for stress analysis of idealized thin walled open sections
by: Syed Mohamed Ali, Jaffar, et al.
Published: (2013)
by: Syed Mohamed Ali, Jaffar, et al.
Published: (2013)
Framework of conceptual design methodology for hybrid buoyant
aircraft
by: UlHaque, Anwar, et al.
Published: (2016)
by: UlHaque, Anwar, et al.
Published: (2016)
Modeling 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)
Similar Items
-
Educational software for stress analysis of non-idealized closed thin-walled sections
by: Syed Mohamed Ali, Jaffar, et al.
Published: (2018) -
Educational software for stress analysis of idealized closed thin walled sections
by: Syed Mohamed Ali, Jaffar, et al.
Published: (2018) -
Aeroelastic passive control optimization of supersonic composite wing with external stores
by: Sulaeman, Erwin, et al.
Published: (2017) -
Software development for aerodynamic characteristics estimation of wing-body combination of aircraft at cubsonic speeds
by: Dahalan, Md. Nizam, et al.
Published: (2001) -
Design of IIUM aircraft fuselage using composite material
by: Aminanda, Yulfian, et al.
Published: (2011)