Aircraft Engineering and Aerospace Technology: Volume 90 Issue 1
Strapline:
An International JournalTable of contents
An assessment of flight efficiency based on the point merge system at metroplex airports
Ozlem Sahin, Oznur Usanmaz, Enis T. TurgutMetroplex is a system of two or more airports, in physical proximity, with highly interdependent arrival and departure operations. The purpose of this study is the construction of…
Thermoelastic flexural analysis of FG-CNT doubly curved shell panel
Kulmani Mehar, Subrata Kumar PandaThe purpose of this paper is to develop a general mathematical model for the evaluation of the theoretical flexural responses of the functionally graded carbon nanotube-reinforced…
In-flight icing risk prediction and management in consideration of wing stall
Binbin Pei, Haojun Xu, Yuan Xue, Wei Chen, Anwei ShenThe purpose of this work is to develop an in-flight icing risk assessment methodology by quantification of changing flight dynamic characteristics under icing conditions.
On-orbit frequency identification of spacecraft based on attitude maneuver data
Yong Xie, Pan Liu, Guoping CaiThe purpose of this paper is to present an on-orbit frequency identification method for spacecraft directly using attitude maneuver data. Natural frequency of flexible solar…
Ring gyroscope sensitive element based on nanoporous alumina
Gennady Gorokh, Yauhen Belahurau, Anna Zakhlebayeva, Igor Taratyn, Viatcheslav KhatkoThis paper aims to present new technological approaches of manufacturing of micromechanical gyroscope ring-sensitive element based on the nanoporous anodic alumina instead of…
Aircraft wing design at low speeds using Taguchi method
Mustafa Soylak, Nurseda Karagöz Gökçe, Eyüp Sabri TopalThe purpose of this paper is to determine the impact level of parameters affecting wing design at low speeds using Taguchi method.
Backstepping sliding mode control for formation flying spacecraft
Yong Guo, Shen-Min Song, Xue-Hui LiThis paper aims to investigate the problem of finite-time consensus tracking control without unwinding for formation flying spacecraft in the presence of external disturbances.
New fault-tolerant federated Kalman filters for integrated navigation
Yueqian Liang, Yingmin JiaThe purpose of this paper is to achieve accurate integrated navigation results for the unmanned aerial vehicle (UAV) systems even in the presence of possible navigation faults in…
Effect of J3 perturbation on satellite position in LEO
Nai-ming Qi, Qilong Sun, Yong YangThe purpose of this paper is to study the effect of J3 perturbation of the Earth’s oblateness on satellite orbit compared with J2 perturbation.
The effects of dynamic-stall and parallel BVI on cycloidal rotor
Yu Hu, Hailang Zhang, Gengqi WangThis paper aims to investigate the mechanisms lying behind the cycloidal rotor under hovering status.
Fatigue based design and life estimation of viscoelastic rotors
Haraprasad Roy, Abhinav Khare, Saurabh Chandraker, J.K. DuttHigh-speed rotor subjected to cyclic stress during operation may cause fatigue failure. Thus, the design of a rotor-shaft should involve the fatigue analysis for predicting safe…
Orbital perturbation due to orbit-attitude coupling near asteroids
Yue Wang, Rui Zhong, Shijie XuThe purpose of this paper is to assess the orbital perturbation caused by the gravitational orbit–attitude coupling of spacecraft in the proximity of asteroids.
Comparison of 1D and 3D thermal models of the nacelle ventilation system in a small airplane
Piotr Łapka, Marije Bakker, Piotr Furmański, Hans van TongerenInsight in the temperature distribution on the internal and external surface of the nacelle is of great importance during the design phase of an aircraft. However, detailed…
Large eddy simulation of airfoil self-noise using OpenFOAM
Hasan Kamliya Jawahar, Yujing Lin, Mark SavillThe purpose of this paper is to investigate airfoil self-noise generation and propagation by using a hybrid method based on the large-eddy simulation (LES) approach and Curle’s…
The influence of the cutting edge shape on high performance cutting
Jan Burek, Lukasz Zylka, Marcin Plodzien, Michal Gdula, Pawel SulkowiczThe purpose of this paper is to determine the influence of the shape of a cutting edge on high-performance milling high-performance cutting. The main purpose of the test was to…
Five-axis milling of sculptured surfaces of the turbine blade
Michal Gdula, Jan Burek, Lukasz Zylka, Marcin PlodzienThe purpose of this paper is to determine the influence of a toroidal cutter axis orientation and a variable radius of curvature of the machined contour of sculptured surface on…
Pilot error in process of helicopter starting
Evica Stojiljkovic, Bojan Bijelic, Miroljub Grozdanovic, Marko Radovanovic, Igor DjokicThe purpose of this paper is to identify potential helicopter pilots’ errors during their interaction with the flight deck in the process of starting a helicopter in night-time…
Decentralized control for spacecraft formation in elliptic orbits
Baolin Wu, Xibin CaoThis paper aims to address the problem of formation control for spacecraft formation in elliptic orbits by using local relative measurements.
Computational modeling of the flow in a wind tunnel
Mahmood Khalid, Khalid A. Juhany, Salah HafezThe purpose of this paper is to use a computational technique to simulate the flow in a two-dimensional (2D) wind tunnel where the effect of the solid walls facing the model has…
Adaptive robust control of coupled attitude and orbit for spacecraft with model uncertainties
Jun Sun, Xiande Wu, Shijie Zhang, Fengzhi Guo, Ting SongThe purpose of this paper is to propose an adaptive robust controller for coupled attitude and orbit control of rigid spacecraft based on dual quaternion in the presence of…
A simplified model for predicting the propeller-wing interaction
Xianghua Huang, Xiaochun Zhao, Jiaqin HuangThe traditional numerical methods to predict the interaction between the wing and propeller are too complex and time-consuming for computation to a certain extent. Therefore, they…
Utilization PPP method in aircraft positioning in post-processing mode
Kamil Krasuski, Damian Wierzbicki, Henryk JafernikThe purpose of this paper is to study the implementation of GNSS technique in aviation for recovery of aircraft’s position using Precise Point Positioning (PPP) method.
Flight test of fault-tolerant flight control system using simple adaptive control with PID controller
Hidenobu Matsuki, Taishi Nishiyama, Yuya Omori, Shinji Suzuki, Kazuya Masui, Masayuki SatoThis paper aims to demonstrate the effectiveness of a fault-tolerant flight control method by using simple adaptive control (SAC) with PID controller.
Modeling and control for ultra-low altitude cargo airdrop
Yanhua HanThe purpose of this paper is to model the aircraft-cargo’s coupling dynamics during ultra-low altitude heavy cargo airdrop and to design the aircraft’s robust flight control law…
Aircraft test of engineered material arresting system
Hong-Yu Yao, Xiang-Jun Kong, Ya-Jie Shi, Xian-Bo Xiao, Ning-Ning LeEngineered material arresting systems (EMASs) are dedicated to stopping aircraft that overrun the runway before they enter dangerous terrain. The system consists of low-strength…
ISSN:
0002-2667Online date, start – end:
1929Copyright Holder:
Emerald Publishing LimitedOpen Access:
hybridEditor:
- Prof Phil Webb