Aircraft Engineering and Aerospace Technology: Volume 90 Issue 9
Strapline:
An International JournalTable of contents
Efficient structural analysis of gas turbine blades
Timo Rogge, Ricarda Berger, Linus Pohle, Raimund Rolfes, Jörg WallaschekThe purpose of this study a fast procedure for the structural analysis of gas turbine blades in aircraft engines. In this connection, investigations on the behavior of gas turbine…
Vibration suppression of a thermoelastic FGM beam subjected to follower force
Mohammad AzadiThe purpose of this paper is to analyze and control the flutter vibrations of a thermoelastic functionally graded material (FGM) beam subjected to follower force using the…
Constrained control of helicopter vibration to reduce motion blur
Tugrul Oktay, Harun Celik, Ilke TurkmenThe purpose of this paper is to examine the success of constrained control on reducing motion blur which occurs as a result of helicopter vibration.
Interactive processing of radar target detection and tracking
Weishi ChenAn interactive processing scheme is proposed to improve the target detection probability as well as the tracking performance of the radar system.
Designing flow chart for aircraft type training in aviation training process management
Ebru Yazgan, Ayşe Kucuk YilmazTraining management has critical in developing of civil aviation sector in Turkey. It requires using serious corporate sources for this reason is directly topic of aviation…
Aerodynamic characteristics of helicopter engine side air intakes
Florian Knoth, Christian BreitsamterAerodynamic characteristics of engine side air intakes for a lightweight helicopter are investigated aiming to achieve an efficient engine airframe integration.
Flow field and acoustics characteristics of elliptical jet
S. Manigandan, Vijayaraja K.The purpose of this paper is to present the results of mixing promotion and screech frequency of controlled elliptical supersonic jet.
Analysis of natural fibre composites for aerospace structures
Salvatore BrischettoThe main idea is the comparison between composites including natural fibres (such as the linoleum fibres) and typical composites including carbon fibres or glass fibres. The…
Topology optimization of a novel fuselage structure in the conceptual design phase
Dianzi Liu, Chuanwei Zhang, Z. Wan, Z. DuIn recent years, innovative aircraft designs have been investigated by researchers to address the environmental and economic issues for the purpose of green aviation. To keep air…
Corporate performance management: process of organizational-tailored flow chart
Ayşe Kucuk Yilmaz, Ebru YazganMain issue in management and strategy is corporate performance. Managers seek effective and strategic way to improve their performance. Authorization, which includes reputational…
A distributed and integrated method for cooperative mission planning of multiple heterogeneous UAVs
Weinan WU, Naigang CuiThe purpose of this paper is to develop a distributed and integrated method to get a fast and feasible solution for cooperative mission planning of multiple heterogeneous unmanned…
Aircraft positioning using PPP method in GLONASS system
Kamil Krasuski, Janusz C´wiklak, Henryk JafernikThe purpose of the study is focused on implementation of Global Navigation Satellite System (GLONASS) technique in civil aviation for recovery of aircraft position using Precise…
Investigation on the benefit of formation flight with a focus on the leading and trailing aircraft rotation
Yaolong Liu, Yaoming ZhouThe purpose of this paper is to study the potential advantages of aircraft formation flight (FF) and to exploit further benefits through exchanging the leading positions.
Hardware-in-the-loop flight motion simulation of flexible variable sweep aircraft
Irum Inayat, Rooh ul Amin, Malik Mazhar AliThis paper aims to propose an improved and computationally efficient motion simulation of a flexible variable sweep aircraft.
Maximum lift/drag ratio improvement of TUAVs via small aerodynamic modifications
Tugrul Oktay, Metin Uzun, Ozturk Ozdemir KanatThe purpose of this study is to increase maximum lift/drag ratio (Emax) of tactical unmanned aerial vehicles (TUAVs) via applying novel small aerodynamic modifications.
Application of virtual flight test framework with derivative design optimization
Hyeong-Uk Park, Joon Chung, Ohyun KwonThe purpose of this paper is a development of a virtual flight test framework with derivative design optimization. Aircraft manufactures and engineers have been putting…
Distributed task allocation for multiple heterogeneous UAVs based on consensus algorithm and online cooperative strategy
Weinan Wu, Naigang Cui, Wenzhao Shan, Xiaogang WangThe purpose of this paper is to develop a distributed task allocation method for cooperative mission planning of multiple heterogeneous unmanned aerial vehicles (UAVs) based on…
Propeller thrust force contribution to airplane longitudinal stability
Miodrag Milenković-BabićThis paper aims to present the new information about propeller thrust force contribution to airplane longitudinal stability analysis.
Control of pendular motion on tethered satellites systems
Paul Kimutai Tirop, Zhang JingruiThis paper aims to present the control laws to be used in the control of pendular motion on tethered satellite systems in space during orbiting by using a nonlinear design…
Development of a testing methodology for high-altitude propeller
Jun Jiao, Bifeng Song, Yubin Li, Yugang Zhang, Jianhua XuThe purpose of this paper is to develop a propeller performance measurement method for high-altitude platforms by analyzing of the propeller aerodynamic characteristics and…
ISSN:
0002-2667Online date, start – end:
1929Copyright Holder:
Emerald Publishing LimitedOpen Access:
hybridEditor:
- Prof Phil Webb