Aircraft Engineering and Aerospace Technology: Volume 91 Issue 7
Strapline:
An International JournalTable of contents
Real-time integrated turboprop take-off model under propeller-wing interaction
Yiwei Wang, Xianghua Huang, Jiaqin HuangThe purpose of the paper is to build a real-time integrated turboprop take-off model which fully takes the interaction between diverse parts of aircraft into consideration…
Solar UAV design framework for a HALE flight
Hoyon Hwang, Jaeyoung Cha, Jon AhnThe purpose of this paper is to present the development of an optimal design framework for high altitude long endurance solar unmanned aerial vehicle. The proposed solar aircraft…
Challenges of turboprop engine installation on small aircraft
Paweł Guła, Dawid Ulma, Krzysztof Żurek, Rafał ŻurawskiThe purpose of this paper is to present the challenges of turbine engine installation on small aircraft. The work was a part of the European Union project Efficient Systems and…
Simulation of active cancellation system based on N-order SSC algorithm
Yacong Wu, Jun Huang, Mingxu Yi, Chaopu ZhangThe purpose of this paper is to introduce the theoretical basis of N-order spectral spreading-compressing (SSC) frequency shift interference algorithm and expand it to active…
High-precision navigation and positioning of celestial exploration rover based on depth camera
Chengchao Bai, Jifeng Guo, Hongxing ZhengThe purpose of this paper is to verify the correctness and feasibility of simultaneous localization and mapping (SLAM) algorithm based on red-green-blue depth (RGB-D) camera in…
Numerical investigation on operation characteristic of ramjet projectile
Chang-Fei Zhuo, Ming-Xiao Wang, Wen-Jin Yao, Wen-ke XuThe purpose of this paper is to study the operation performance of the high-speed ramjet kinetic energy projectile using solid fuel ramjet as power plant that is a new short-range…
Reachable domain of spacecraft with a single normal impulse
Junhua Zhang, Jianping Yuan, Wei Wang, Jiao WangThe purpose of this paper is to obtain the reachable domain (RD) for spacecraft with a single normal impulse while considering both time and impulse constraints.
LCA of the maintenance of a piston-prop engine
Yasin Şöhret, Selcuk Ekici, Onder Altuntas, T. Hikmet KarakocThis study aims to introduce an approach to evaluate environmental impact of a piston-prop engine from the view point of life cycle assessment (LCA).
A novel improvement of Kriging surrogate model
Wei He, Yuanming Xu, Yaoming Zhou, Qiuyue LiThis paper aims to introduce a method based on the optimizer of the particle swarm optimization (PSO) algorithm to improve the efficiency of a Kriging surrogate model.
Study on multi-loop control strategy of three-shaft gas turbine for electricity generation
Zilai Zhang, Shusheng Zang, Bing GeThis paper aims to develop a dynamic performance model of three-shaft gas turbine for electricity generation and to study a multi-loop control strategy of three-shaft gas turbine…
Influences of airfoil profile on lateral-directional stability of aircraft with flying wing layout
Yalin Pan, Jun HuangThe purpose of this study is to analyze influence of airfoil profile on lateral-directional flying quality of flying wing aircraft. The lateral-directional stability is always…
Dynamics and control of a flexible rotating clamped-free beam by SDRE strategy
Vinicius Piro Barragam, Andre Fenili, Ijar Milagre da FonsecaThe purpose of this paper is the dynamic analysis of the coupled rotation and vibration motion of a system containing a central rigid body to which is attached a flexible beam.
Short range rocket-target: research, development and implementation
Algimantas Fedaravičius, Sigitas Kilikevičius, Arvydas Survila, Saulius RačkauskasThe purpose of this paper is to present the aerodynamic analysis and external ballistics modeling used in the development of a rocket-target for short range air defence missile…
Aircraft flow angles calibration via observed-based wind estimation
Francesco Schettini, Gianpietro Di Rito, Eugenio DentiThis paper aims to propose a novel approach, in which the reference data for the flow angles calibration are obtained by using measurements coming from an inertial navigation…
Thermally induced dynamics of deployable solar panels of nanosatellite
Syahrim Azhan Ibrahim, Eiki YamaguchiThis study aims to predict the types of thermally induced dynamics (TID) that can occur on deployable solar panels of a small form factor satellite, CubeSat which flies in low…
An integrated solution for space shuttle launching ramp
G. Nilay Yücenur, Anıl Sezer SubaşıThe purpose of this study is to select the most appropriate city in Turkey for space shuttle launching ramp.
Flow separation control of NACA-2412 airfoil with bio-inspired nose
Mohamed Arif Raj Mohamed, Ugur Guven, Rajesh YadavThe purpose of this paper is to achieve an optimum flow separation control over the airfoil using passive flow control method by introducing bio-inspired nose near the leading…
Design-airworthiness integration method for general aviation aircraft during early development stage
Maxim Tyan, Jungwon Yoon, Nhu Van Nguyen, Jae-Woo Lee, Sangho KimMajor changes of an aircraft configuration are conducted during the early design stage. It is important to include the airworthiness regulations at this stage while there is…
ISSN:
0002-2667Online date, start – end:
1929Copyright Holder:
Emerald Publishing LimitedOpen Access:
hybridEditor:
- Prof Phil Webb