Aircraft Engineering and Aerospace Technology: Volume 93 Issue 5
Strapline:
An International JournalTable of contents
Online monitoring experiments of turbo-shaft engine based on electrostatic sensor
Jiachen Guo, Heng Jiang, Zhirong Zhong, Hongfu Zuo, Huan ZhangElectrostatic monitoring technology is a useful tool for monitoring and detecting component faults and degradation, which is necessary for engine health management. This paper…
Aerodynamic ground effects on DLRF6 vehicle
Mojtaba Tahani, Mehran Masdari, Ali BargestanThe overall performance of an aerial vehicle strongly depends on the specifics of the propulsion system and its position relative to the other components. The purpose of paper is…
Numerical study on trajectory of released store with manipulation of grid connections
Mohammad Mehdi RazzaghiThis study aims to present a moving grid method based on the manipulation of connections.
An analytical model of the replacement costs of aircraft engine life-limited parts
Branimir Stojiljković, Ljubiša Vasov, Olja Čokorilo, Goran VorotovićThe purpose of this paper is to present novel recursive expressions for modelling the replacement costs of aircraft engine life-limited parts during shop visits to assist engine…
Ground simulation of fuel cell/battery hybrid propulsion system for small unmanned air vehicles
Sinan Keiyinci, Kadir AydinThe endurance of small unmanned air vehicles (UAVs) is directly associated with the energy density of the propulsion system used. As the batteries commonly used in small UAVs have…
Ontology modelling of intelligent HCI in aircraft cockpit
Xia Zhang, Youchao Sun, Yanjun ZhangSemantic modelling is an essential prerequisite for designing the intelligent human–computer interaction in future aircraft cockpit. The purpose of this paper is to outline an…
Structural optimization of a composite launch tube of man portable air defense system
Efecan Yar, Erdem AcarThe purpose of this paper is to find the optimum configuration of the composite launch tube currently being developed in Roketsan. The winding thicknesses and winding angles of…
A comprehensive performance optimization method for the honeycomb buffer of a legged-type lander
Hui Wang, Tianyu He, Chunjie WangIn the field of planetary exploration, the legged-type lander is a common landing buffer device. There are two important performance metrics for legged-type landers: the energy…
UAV icing: the influence of airspeed and chord length on performance degradation
Richard Hann, Tor Arne JohansenThe main purpose of this paper is to investigate the effects of icing on unmanned aerial vehicles (UAVs) at low Reynolds numbers and to highlight the differences to icing on…
Integration effects of UAVs in non-segregated airspace
Tamer Savas, Oznur Usanmaz, Ozlem Sahin, Ertan Çınar, Murat KaraderiliThe study aims to design a new route model for unmanned aerial vehicles (UAVs) to integrate them into non-segregated airspace.
Adaptive rapid neural observer-based sensors fault diagnosis and reconstruction of quadrotor unmanned aerial vehicle
Muhammad Taimoor, Xiao Lu, Hamid Maqsood, Chunyang ShengThe objective of this research is to investigate various neural network (NN) observer techniques for sensors fault identification and diagnosis of nonlinear system in…
High accuracy disturbance observer-based agile attitude stabilization with three-dimensional MSW
Javad Tayebi, Chao Han, Yuanjin YuThe purpose of this paper is agile attitude control design with the novel three-dimensional (3D) magnetically suspended wheel (MSW) that is the preferred type for agile…
An improved ellipsoid optimization algorithm in subspace predictive control
Wang JianhongThe purpose of this paper is to derive the output predictor for a stationary normal process with rational spectral density and linear stochastic discrete-time state-space model…
Computation of dimensional variations on the structural analysis of multi-cell aircraft box beams with python scripting
Hande YavuzPython codes are developed for the versatile structural analysis on a 3 spar multi-cell box beam by means of idealization approach.
Aeroacoustic and aerodynamic characteristics of a morphing airfoil
Zi Kan, Daochun Li, Shiwei Zhao, Jinwu Xiang, Enlai ShaThis paper aims to assess the aeroacoustic and aerodynamic performance of a morphing airfoil with a flexible trailing edge (FTE). The objective is to make a comparison of the…
Free vibration analysis of a rotating double tapered beam with flexible root via differential quadrature method
Mustafa Tolga Tolga Yavuz, İbrahim ÖzkolThis study aims to develop the governing differential equation and to analyze the free vibration of a rotating non-uniform beam having a flexible root and setting angle for…
Prediction of lean blowout performance on variation of combustor inlet area ratio for micro gas turbine combustor
Kirubakaran V., Naren Shankar R.This paper aims to predict the effect of combustor inlet area ratio (CIAR) on the lean blowout limit (LBO) of a swirl stabilized can-type micro gas turbine combustor having a…
Computational analysis to enhance the compressible flow over an aerofoil surface
Siva Marimuthu, Dhavamani ChinnathambiSince the inception of aerospace engineering, reducing drag is of eternal importance. Over the years, researchers have been trying to improve the aerodynamics of National Advisory…
ISSN:
0002-2667Online date, start – end:
1929Copyright Holder:
Emerald Publishing LimitedOpen Access:
hybridEditor:
- Prof Phil Webb