Aircraft Engineering and Aerospace Technology: Volume 77 Issue 1
Strapline:
An International JournalTable of contents
International space station mechanism contact simulation
Jan P. FaveroTo provide an overview of how the solid‐to‐solid contact force equation in MSC.ADAMS can be used to reduce contact model development, minimize the probability of introducing an…
Feedforward neural network based non‐linear dynamic modelling of a TRMS using RPROP algorithm
M. Hasan ShaheedTo develop a non‐linear modelling technique for modern air vehicles with an application to a twin rotor multi‐input‐multi‐output system (TRMS) which resembles the dynamics of a…
Kalman filter and neural network‐based icing identification applied to A340 aircraft dynamics
Rahmi Aykan, Chingiz Hajiyev, Fikret ÇalişkanThe purpose of this paper is to maintain safe flight and to improve existing deicing (in‐flight removal of ice) and anti‐icing (prevention of ice accretion) systems under…
Investigation of a 3D non‐contact measurement based blade repair integration system
Jian Gao, Janet Folkes, Oguzhan Yilmaz, Nabil GindyThe aim of the paper is to provide an economically viable solution for the blade repair process. There is a continual increase in the repair market, which requires an increased…
On‐line monitoring and diagnosis for satellite telemetry data
Bing Long, Zhengji Song, Xingwei JiangTo improve the speed and precise of online monitoring and diagnosis for satellite using satellite telemetry data.Design/methodology/approach – In monitoring system, a fuzzy range…
Dynamic stability characteristics of doubly curved panels with circular cutout subjected to follower edge load
L. Ravi Kumar, P.K. Datta, D.L. PrabhakaraTo predict the critical flutter load and frequencies of doubly curved panels using first‐order shear deformation theory considering the effects of shear deformation and rotary…
Analyses on ducted tail rotor and airfoil aerodynamic characteristics with CFD
Yihua Cao, Ke Chen, Jian WangTo establish a method for the calculations in the field of rotor aerodynamics.Design/methodology/approach – The calculations of the lift‐drag characteristics of OAF and NACA63A312…
ISSN:
0002-2667Online date, start – end:
1929Copyright Holder:
Emerald Publishing LimitedOpen Access:
hybridEditor:
- Prof Phil Webb