On the evaluation of negative altitude requirement for flutter speed boundary of transport aircraft and UAV

QR Code

On the evaluation of negative altitude requirement for flutter speed boundary of transport aircraft and UAV

To maintain flight safety, all transport aircraft designs should satisfy airworthiness standard regulation. One fundamental issue of the aircraft design that relates directly to flight safety as well as commercial aspect of the aircraft is on the evaluation of the maximum speed within the designa...

Full description

Bibliographic Details
Main Author:	Sulaeman, Erwin
Format:	Article
Language:	English
Published:	Trans Tech Publications Ltd., Switzerland 2012
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/34462/ http://irep.iium.edu.my/34462/1/AMM.225.397.pdf

Similar Items

Flutter analysis of supersonic wing with external stores
by: Abdullah, Nur Azam, et al.
Published: (2013)

Aeroelastic flutter analysis of supersonic wing with multiple external stores
by: Abdullah, Nur Azam, et al.
Published: (2014)

Literature review : Biomimetic and conventional aircraft wing tips
by: Ahmed Siddiqui, Naseeb, et al.
Published: (2017)

Hybrid buoyant aircraft: future STOL aircraft for interconnectivity of the Malaysian islands
by: UlHaque, Anwar, et al.
Published: (2017)

Framework of conceptual design methodology for hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2016)

Stability and takeoff ground roll issues of hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2014)

Establishing the analytical relationships for mass and volumetric mass fractions for hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2016)

Half model testing for canard of a hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2015)

Assessment of engine's power budget for hydrogen powered hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2016)

Aerostatic and aerodynamic modules of a hybrid buoyant aircraft: an analytical approach
by: UlHaque, Anwar, et al.
Published: (2015)

Effect of wing loading on gross takeoff mass of a hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2016)

Effect of side wind on the directional stability and aerodynamics of a hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2016)

Establishing the analytical relationships for mass and volumetric mass fractions for hybrid boyant aircraft
by: UlHaque, Anwar, et al.
Published: (2015)

Power-off static stability analysis of a clean configuration of a hybrid buoyant aircraft
by: Ul Haque, Anwar, et al.
Published: (2015)

Accurate geometric stiffness matrix formulation of beam finite element
by: Sulaeman, Erwin
Published: (2011)

Axial stiffness matrix of non-uniform Bernoulli-Euler bar element
by: Sulaeman, Erwin
Published: (2011)

Evaluation of aircraft wing-tip vortex using PIV
by: Elsayed, Omer Ali, et al.
Published: (2009)

Approximate function for unsteady aerodynamic kernel function of aeroelastic lifting surfaces
by: Sulaeman, Erwin, et al.
Published: (2014)

Alternate approximate function for kernel function of oscillating lifting surfaces
by: Sulaeman, Erwin, et al.
Published: (2013)

The aerodynamics analysis of type UAV aircraft with pusher engine configuration by use of DATCOM software
by: Al Aian, Ahmad Eshtiwey
Published: (2011)

Experimental investigation of free wing IIUM-UAV configuration
by: Omar, Ashraf Ali, et al.
Published: (2010)

Aeroelastic tailoring of oscillating supersonic wing with external stores
by: Abdullah, Nur Azam, et al.
Published: (2014)

Educational software for stress analysis of an aircraft fuselage
by: Mohamed Ali, Jaafar Syed, et al.
Published: (2010)

Low reynolds number numerical simulation of the aerodynamic coefficients of a 3D wing
by: Malik, Khurshid, et al.
Published: (2018)

Crash analysis of an aircraft fuselage under belly landing
by: Syed Mohamed Ali, Jaffar, et al.
Published: (2017)

Performance evaluation of linear quadratic regulator and linear quadratic Gaussian controllers on quadrotor platform
by: Islam, Maidul, et al.
Published: (2019)

Flutter assessment on composite plate with crack by means of fully coupled Finite Element and Doublet Lattice Method
by: Abdullah, Nur Azam, et al.
Published: (2017)

CFD analysis on the effect of winglet cant angle on aerodynamics of ONERA M6 wing
by: Munshi, Adnan, et al.
Published: (2018)

Roll control reversal of variable swept wing in supersonic flow
by: Ibren, Mohamed, et al.
Published: (2019)

Experimental investigation of a new spiral wingtip
by: Siddiqui, Naseeb, et al.
Published: (2018)

Effect of diamond shaped strut with cylindrical pitch rod in subsonic wind tunnel testing
by: UlHaque, Anwar, et al.
Published: (2017)

Wind tunnel testing on a generic model of a hybrid lifting hull
by: UlHaque, Anwar, et al.
Published: (2016)

Prediction of buckling mode for simply supported stiffened thin plates subject to inplane loading
by: Abdul Halim, Abdul Karim, et al.
Published: (2019)

Analysis on cracked commuter aircraft wing under dynamic cruise load by means of XFEM
by: Wirawan, Nanda, et al.
Published: (2018)

Prediction of aerodynamic characteristics of an aircraft model with and without winglet using fuzzy logic technique
by: Hossain, Altab, et al.
Published: (2011)

A review on aerodynamics of nonflapping bird wings
by: Mohammed Aldheeb, Mohammed Abdulmalek, et al.
Published: (2016)

Aerodynamics of porous airfoils and wings
by: Mohammed Aldheeb, Mohammed Abdulmalek, et al.
Published: (2018)

Investigation On The Propulsive Efficiency Of The Small Uav Conceptual Design
by: Yahya, Khairul Ikhsan
Published: (2012)

Flutter Modeling And Simulation Of Wing Section Using Bondgraph Technique [TL574.F6 N841 2005 f rb] [Microfiche 8089].
by: Abdul Razak, Norizham
Published: (2005)

Yawing force of electric trimmers of a hybrid buoyant aerial vehicle
by: UlHaque, Anwar, et al.
Published: (2017)