Aircraft Engineering and Aerospace Technology: Volume 92 Issue 4

Mechanical properties of near alpha titanium alloys for high-temperature applications - a review

Vitus Mwinteribo Tabie, Chong Li, Wang Saifu, Jianwei Li, Xiaojing Xu

This paper aims to present a broad review of near-a titanium alloys for high-temperature applications.

Exploring experiential indicators in flight training organization: a case study

Vehbi Emrah Atasoy, Selcuk Ekici

The purpose of this paper is to introduce an approach to evaluate the establishment requirements of an flight training organization (FTO) through indicators that are not included…

A review on the applications of the chemical reactor network approach on the prediction of pollutant emissions

Hamidreza Khodayari, Fathollah Ommi, Zoheir Saboohi

The purpose of this paper is to review the applications of the chemical reactor network (CRN) approach for modeling the combustion in gas turbine combustors and classify the CRN…

Simulation of dielectric barrier discharge actuator at low Reynolds number

Nima Vaziri, Ming-Jyh Chern, Tzyy-Leng Horng, Syamsuri Syamsuri

The purpose of this study is to the modeling of the dielectric barrier discharge (DBD) actuator on the Eppler 387 (E387) airfoil in low Reynolds number conditions.

Simultaneous determination of maximum acceleration and endurance of morphing UAV with ABC algorithm-based model

Mehmet Konar

The purpose of this paper is to present a novel approach based on the artificial bee colony (ABC) algorithm aiming to achieve maximum acceleration and maximum endurance for…

Spacecraft formation control using aerodynamic and Lorentz force

Ran Sun, Aidang Shan, Chengxi Zhang, Qingxian Jia

This paper aims to investigate the feasibility of using the combination of Lorentz force and aerodynamic force as a propellantless control method for spacecraft formation.

LPV robust servo control of aircraft active side-sticks

Guang Rui Zhou, Shi Qian Liu, Yuan Jun Sang, Xu Dong Wang, Xiao Peng Jia, Er Zhuo Niu

This paper aims to focus on the variable stick force-displacement (SFD) gradience in the active side stick (ASS) servo system for the civil aircraft.

Transition effect on aerodynamic performance of compressor profile

Ryszard Szwaba, Piotr Kaczyński, Piotr Doerffer

The purpose of this paper is to study experimentally the effect of transition and also the roughness height on the flow structure of the shock wave boundary layer interaction in…

Simulation studies of a vision intruder detection system

Paweł Rzucidło, Tomasz Rogalski, Grzegorz Jaromi, Damian Kordos, Piotr Szczerba, Andrzej Paw

The purpose of this paper is to describe simulation research carried out for the needs of multi-sensor anti-collision system for light aircraft and unmanned aerial vehicles.

Characteristics of a co-flowing jet with varying lip thickness and constant velocity ratio

Naren Shankar R., Kevin Bennett S., Dilip Raja N., Sathish Kumar K.

This study aims to analyze co-flowing jets (CFJs) with constant velocity ratio (VR) and varying primary nozzle lip thickness (LT) to find a critical LT in CFJs below which mixing…

Autonomous performance maximization of research-based hybrid unmanned aerial vehicle

Sezer Çoban

This paper aims to investigate the autonomous performance optimization of a research-based hybrid unmanned aerial vehicle (i.e. HUAV) manufactured at Iskenderun Technical…

Dynamic analysis of a double-helical geared rotor system with oil-film bearing

Ying-Chung Chen, Tsung-Hsien Yang, Siu-Tong Choi

This paper aims to study a dynamic analysis of a double-helical geared rotor system with oil-film bearing.