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Research article

First published 2019-12

Composite adaptive posicast controller for the wing rock phenomenon in a delta-wing aircraft

Amir Yousefimanesh, Alireza Khosravi, Pouria Sarhadi

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2011-4

Stability derivatives for a delta-wing X-31 aircraft validated using wind tunnel test data

N Anton, R M Botez, D Popescu

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Other

First published 2003-05

A Multidisciplinary Analysis of Tail Buffeting Alleviation Using Streamwise Fences

Essam F. Sheta

Journal of Vibration and Control

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Research article

First published 2002-4

Non-linear modelling of a one-degree-of-freedom twin-rotor multi-input multi-output system using radial basis function networks

S M Ahmad, M H Shaheed, A J Chipperfield [...]

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

Open access

Research article

First published 2017-7

Investigation of wing structure layout of aerospace plane based on the finite element method

Yu Wang, Lei Liu, Yu Xing [...]

Advances in Mechanical Engineering

Open access

Research article

First published 2016-9

A miniature seven-hole probe air data system and its application on spin prediction

Shaoze Li, Yunsong Gu, Jiexing Han [...]

International Journal of Micro Air Vehicles

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Research article

First published 2006-5

Continuing evolution of aerodynamic concept development using collaborative numerical and experimental evaluations

R M Cummings, S A Morton

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

Search results

Composite adaptive posicast controller for the wing rock phenomenon in a delta-wing aircraft

Stability derivatives for a delta-wing X-31 aircraft validated using wind tunnel test data

A Multidisciplinary Analysis of Tail Buffeting Alleviation Using Streamwise Fences

Non-linear modelling of a one-degree-of-freedom twin-rotor multi-input multi-output system using radial basis function networks

Investigation of wing structure layout of aerospace plane based on the finite element method

A miniature seven-hole probe air data system and its application on spin prediction

Continuing evolution of aerodynamic concept development using collaborative numerical and experimental evaluations