Browsing by Author "Guo, Shijun J."

Optimal design and numerical analysis of a morphing flap structure

Di Matteo, Natalia (Cranfield University, 2012-10)

Over the next few years the aviation industry will face the challenge to develop a new generation of air vehicles characterised by high aerodynamic efficiency and low environmental impact. The technologies currently ...

Optimal design of a composite active aeroelastic wing

Perera, Melanie (Cranfield University, 2011-02)

The primary aim of this research was to design a Seamless Aeroelastic Wing (SAW) structure applicable to a lightweight Unmanned Aerial Vehicle (UAV). Therefore the study focused on optimal design of a SAW structure by ...

Optimal design of a composite wing structure for a flying-wing aircraft subject to multi-constraint

Xu, Rongxin. (Cranfield University, 2012-01)

This thesis presents a research project and results of design and optimization of a composite wing structure for a large aircraft in flying wing configuration. The design process started from conceptual design and preliminary ...

Optimal design of a flying-wing aircraft inner wing structure configuration

Huang, Haidong (Cranfield University, 2012-01)

Flying-wing aircraft are considered to have great advantages and potentials in aerodynamic performance and weight saving. However, they also have many challenges in design. One of the biggest challenges is the structural ...

Optimal design of an aeroelastic wing structure with seamless control surfaces

Perera, Melanie; Guo, Shijun J. (Professional Engineering Publishing, 2009-08-01)

This article presents an investigation into the concept and optimal design of a lightweight seamless aeroelastic wing (SAW) structure for small air vehicles. Attention has been first focused on the design of a hingeless ...

Optimization of a Composite Wing Subject to Multi Constraints

Fu, Qiang (Cranfield University, 2013-05)

In this thesis, an investigation has been carried out into a minimum weight optimization analysis of a composite wing with multi design constraints under both static and dynamic loadings. The study includes the influence ...

Optimum buckling design of composite stiffened panels using ant colony algorithm

Wang, Wei; Guo, Shijun J.; Chang, Nan; Yang, Wei (Elsevier Science B.V., Amsterdam., 2010-02-01)

Optimal design of laminated composite stiffened panels of symmetric and balanced layup with different number of T-shape stiffeners is investigated and presented. The stiffened panels are simply supported and subjected to ...

Optimum design of a composite outer wing subject to stiffness and strength constraints

Liu, Yifei (Cranfield University, 2011-01)

Composite materials have been more and more used in aircraft primary structures such as wing and fuselage. The aim of this thesis is to identify an effective way to optimize composite wing structure, especially the stiffened ...

Potential Flow Based Aerodynamic and Aeroelastic Analysis of flapping Wings

Liani, Evandro (Cranfield University, 2008-03)

The motivation for this research is the importance that the modeling of aerodynamics and aeroelasticity of flapping wings has had in the last decade. The development of flapping wings Micro Air Vehicles (MAV) has captured ...

Rolling active control for an aircraft of seamless aeroelastic wing

Wang, Zhengjie; Yang, Daqing; Guo, Shijun J. (Inderscience Publishers, 2009-12-31)

This paper presents an investigation into the controllability for an aircraft of seamless aeroelastic wing. The research is aimed at the design of control laws for the aircraft rolling by actively operating a pair of an ...

Simultaneous partial topology and size optimization of a wing structure using ant colony and gradient based methods

Wang, Wei; Guo, Shijun J.; Yang, Wei (Taylor & Francis, 2011-04-30)

This article presents a methodology and process for a combined wing configuration partial topology and structure size optimization. It is aimed at achieving a minimum structural weight by optimizing the structure layout ...

Stability and control effectiveness of a seamless aeroelastic wing aircraft.

Yang, Da Qing (2011-04)

Today’s aerospace engineers can design a much lighter aircraft than before thanks to the improved accuracy in the estimation of aerodynamic load and structural strength. But reduction of airframe material has also made the ...

Stress concentration and buckling behaviour of shear loaded composite panels with reinforced cutouts

Guo, Shijun J. (Elsevier Science B.V., Amsterdam., 2007-09-01)

Numerical and experimental studies have been conducted to investigate the effect of reinforcements around cutouts on the stress concentration and buckling behaviour of a carbon/epoxy composite panel under in-plane shear ...

Suppression of stall on high-camber flap using upper-surface blowing

Fang, Li (Cranfield University, 2011-01)

For many years, high-lift devices of an aeroplane have been employed to enhancing the aerodynamic performance of the wing during take-off and landing. But their complex geometries not only increase the design and ...

Trim optimizations of an adaptive tailless aircraft with composite wing

Xie, J.; Yang, Z. C.; Guo, Shijun J. (Trans Tech Publications, 2011-02-28)

This paper investigates aeroelastic tailoring and optimal trailing edge control surface deflection to minimize induced drag for a HALE UAV flying wing configuration. The analysis process is conducted on the Finite ...

Unsteady aerodynamic and optimal kinematic analysis of a micro flapping wing rotor

Li, H.; Guo, Shijun J.; Zhang, Y. L.; Zhou, C.; Wu, J. H. (Elsevier, 2016-12-30)

Inspired by the high performance of rotary and insect flapping wings capable of vertical take-off and landing and hovering (VTOLH), a novel flapping wing rotor (FWR) has been developed by combining the above two types of ...

Browsing by Author "Guo, Shijun J."

Browsing by Author "Guo, Shijun J."

Search CERES

Browse

All of CERES

My Account