Professor Jonathan E Cooper

FAIAA, FREng, BSc(London), PhD(London), FRAeS(Royal Aeronautical Society)

  • BS8 1TR

20062020

Research output per year

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Research Output

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Article (Academic Journal)
2020

Structural Modeling of Compliance-Based Camber Morphing Structures under Transverse Shear Loading

Rivero, A. E., Weaver, P. M., Cooper, J. E. & Woods, B. K. S., 4 Jul 2020, (Accepted/In press) In : AIAA Journal.

Research output: Contribution to journalArticle (Academic Journal)

Testing of Folding Wingtip for Gust Load Alleviation of a Flexible High Aspect Ratio Wing

Cheung, R. C. M., Rezgui, D., Cooper, J. E. & Wilson, T., 11 May 2020, In : Journal of Aircraft. 30 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
29 Downloads (Pure)

Wing stiffness parameterisation for surrogate models

Leong, B., Coggon, S. & Cooper, J., 6 Feb 2020, In : CEAS Aeronautical Journal. 2020

Research output: Contribution to journalArticle (Academic Journal)

2019

Aeroelastics Flight Dynamics Coupling Effects of the Semi Aeroelastic Hinge Device

Castrichini, A., Wilson, T., Salteri, F., Mastroddi ,F., Viceconti, N. & Cooper, J. E., 28 Nov 2019, In : Journal of Aircraft. 9 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
111 Downloads (Pure)

A robust and reliability-based aeroelastic tailoring framework for composite aircraft wings

Othman, M. F., Silva, G. H. C., Cabral, P. H., Prado, A. P., Pirrera, A. & Cooper, J. E., 15 Jan 2019, In : Composite Structures. 208, p. 101-113 13 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
1 Citation (Scopus)
260 Downloads (Pure)

Efficient aeroelastic beam modelling and the selection of a structural shape basis

Howcroft, C., Neild, S., Lowenberg, M. & Cooper, J. E., 1 Jun 2019, In : International Journal of Non-Linear Mechanics. 112, p. 73-84 12 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
78 Downloads (Pure)

Enhanced evolutionary-based optimization techniques applied to a nonlinear landing gear design problem

Tartaruga, I., Cooper, J., Lowenberg, M. & Lemmens, Y., 15 May 2019, (Accepted/In press) In : Journal of Aircraft.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
45 Downloads (Pure)

Fault-tolerant control for commercial aircraft with actuator faults and constraints

Liu, Y., Dong, X., Ren, Z. & Cooper, J., 1 May 2019, In : Journal of the Franklin Institute. 356, 7, p. 3849-3868 20 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
1 Citation (Scopus)
47 Downloads (Pure)

Flutter of Telescopic Span Morphing Wings

Ajaj, R. M., Omar, F. K., Darabseh, T. T. & Cooper, J., 1 Jun 2019, In : International Journal of Structural Stability and Dynamics. 19, 6, 24 p., 1950061.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
1 Citation (Scopus)
117 Downloads (Pure)

Industrially-inspired Gust Loads Analysis of Various Aspect Ratio Wings Featuring Geometric Nonlinearity

Cook, R. G., Calderon, D. E., Cooper, J. E., Lowenberg, M. H. & Neild, S. A., 20 Dec 2019, In : Journal of Aircraft. 57, 1, 16 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
130 Downloads (Pure)

Sizing High-Aspect-Ratio Wings with a Geometrically Nonlinear Beam Model

Calderon, D., Cooper, J., Lowenberg, M., Neild, S. & Coetzee, E., 2 Jun 2019, In : Journal of Aircraft. 56, 4, p. 1455-1470 16 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
1 Citation (Scopus)
115 Downloads (Pure)

Systematic statistical characterisation of stress-life datasets using 3-Parameter distributions

Hoole, J., Sartor, P., Booker, J., Cooper, J., Gogouvitis, X. V. & Schmidt, R. K., 1 Dec 2019, In : International Journal of Fatigue. 129, 15 p., 105216.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
1 Citation (Scopus)
5 Downloads (Pure)
2018

Gust and Ground Loads Integration for Aircraft Landing Loads Prediction

Castrichini, A., Cooper, J., Benoit, T. & Lemmens, Y., Jan 2018, In : Journal of Aircraft. 55, 1, p. 184-194 11 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
1 Citation (Scopus)
271 Downloads (Pure)

Improved aerostructural performance via aeroservoelastic tailoring of a composite wing

Krupa, E. P., Cooper, J. E., Pirrera, A. & Nangia, R., Sep 2018, In : The Aeronautical Journal. 122, 1255, p. 1442-1474 33 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
2 Citations (Scopus)
290 Downloads (Pure)

Numerical Continuation of Limit Cycle Oscillations and Bifurcations in High-Aspect-Ratio Wings

Eaton, A., Howcroft, C., Coetzee, E., Neild, S., Lowenberg, M. & Cooper, J., Sep 2018, In : Aerospace. 5, 3, 18 p., 78.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
4 Citations (Scopus)
363 Downloads (Pure)

On the Geometrically Exact Low Order Modelling of a Flexible Beam: Formulation and Numerical Tests

Howcroft, C., Cook, R., Neild, S., Lowenberg, M., Cooper, J. & Coetzee, E., Aug 2018, In : Proceedings of the Royal Society A: Mathematical, Physical and Engineering Sciences. 474, 2216, 27 p., 20180423 .

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
4 Citations (Scopus)
206 Downloads (Pure)

Parametric structural modelling of fish bone active camber morphing aerofoils

Rivero, A. E., Weaver, P., Cooper, J. & Woods, B. K. S., 1 May 2018, In : Journal of Intelligent Material Systems and Structures. 29, 9, p. 2008-2026 19 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
2 Citations (Scopus)
291 Downloads (Pure)

Reliability-based aeroelastic design of composite plate wings using a stability margin

Scarth, C. & Cooper, J., Apr 2018, In : Structural and Multidisciplinary Optimization. 57, 4, p. 1695-1709 15 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
5 Citations (Scopus)
224 Downloads (Pure)

Slender-Wing Beam Reduction Method for Gradient-Based Aeroelastic Design Optimization

Stodieck, O., Cooper, J., Neild, S., Lowenberg, M. & Iorga, L., Nov 2018, In : AIAA Journal. 56, 11, p. 4529-4545 17 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
2 Citations (Scopus)
255 Downloads (Pure)

Testing of a hinged wingtip device for gust loads alleviation

Cheung, R., Rezgui, D., Cooper, J. & Wilson, T., Sep 2018, In : Journal of Aircraft. 55, 5, 37 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
4 Citations (Scopus)
271 Downloads (Pure)

Uncertainty and sensitivity analysis of bifurcation loci characterizing nonlinear landing-gear dynamics

Tartaruga, I., Cooper, J. E., Lowenberg, M. H., Sartor, P. & Lemmens, Y., Jan 2018, In : Journal of Aircraft. 55, 1, p. 162-172 11 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
4 Citations (Scopus)
269 Downloads (Pure)

Veering and nonlinear interactions of a clamped beam in bending and torsion

Ehrhardt, D. A., Hill, T. L., Neild, S. A. & Cooper, J. E., 3 Mar 2018, In : Journal of Sound and Vibration. 416, p. 1-16 16 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
8 Citations (Scopus)
229 Downloads (Pure)
2017

Aeroelastic Tailoring of a Representative Wing-Box Using Tow-Steered Composites

Stodieck, O., Cooper, J., Weaver, P. & Kealy, P., Apr 2017, In : AIAA Journal. 55, 4, p. 1425-1439 15 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
33 Citations (Scopus)
397 Downloads (Pure)

Aeroelastic tailoring using crenellated skins: modelling and experiment

Francois, G., Cooper, J. & Weaver, P., Feb 2017, In : Advances in Aircraft and Spacecraft Science. 4, 2, p. 93-124 31 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
3 Citations (Scopus)
348 Downloads (Pure)

An extended harmonic balance method based on incremental nonlinear control parameters

Khodaparast, H. H., Madinei, H., Friswell, M. I., Adhikari, S., Coggon, S. & Cooper, J. E., 15 Feb 2017, In : Mechanical Systems and Signal Processing. 85, p. 716-729 14 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
5 Citations (Scopus)
239 Downloads (Pure)

Evaluation of a Compliant Droop-Nose Morphing Wing Tip via Experimental Tests

Vasista, S., Riemenschneider, J., van de Kamp, B., Monner, H. P., Cheung, R., Wales, C. & Cooper, J., Mar 2017, In : Journal of Aircraft. 54, 2, p. 519-534 16 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
14 Citations (Scopus)
492 Downloads (Pure)

Identification of systems containing nonlinear stiffnesses using backbone curves

Londoño Monsalve, J. M., Cooper, J. E. & Neild, S. A., 1 Feb 2017, In : Mechanical Systems and Signal Processing. 84 Part B, p. 116-135 20 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
11 Citations (Scopus)
270 Downloads (Pure)

LQG based model predictive control for gust load alleviation

Liu, X., Sun, Q. & Cooper, J., Dec 2017, In : Aerospace Science and Technology. 71, p. 499-509 11 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
14 Citations (Scopus)
128 Downloads (Pure)

Nonlinear Negative Stiffness Wingtip Spring Device for Gust Loads Alleviation

Castrichini, A., Cooper, J. E., Wilson, T., Carrella, A. & Lemmens, Y., Mar 2017, In : Journal of Aircraft. 54, 2, p. 627-641 15 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
153 Downloads (Pure)

Nonlinear Static Aeroelasticity of High Aspect Ratio Wing Aircraft by FEM and Multibody Methods

Castellani, M., Cooper, J. E. & Lemmens, Y., Mar 2017, In : Journal of Aircraft. 54, 2, p. 548-560 13 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
9 Citations (Scopus)
317 Downloads (Pure)

Preliminary investigation of use of flexible folding wing tips for static and dynamic load alleviation

Castrichini, A., Hodigere Siddaramaiah, V., Calderon, D., Cooper, J., Wilson, T. & Lemmens, Y., Jan 2017, In : Aeronautical Journal. 121, 1235, p. 73-94 23 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
22 Citations (Scopus)
279 Downloads (Pure)
2016

Buckling Alleviation for Joined-Wing Aircraft

Lambert, L. A., Cooper, J. E. & Nangia, R. K., May 2016, In : Journal of Aircraft. 53, 3, p. 811-821 11 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
4 Citations (Scopus)
344 Downloads (Pure)

Flight Loads Prediction of High Aspect Ratio Wing Aircraft using Multibody Dynamics

Castellani, M., Cooper, J. E. & Lemmens, Y., 27 Dec 2016, In : SAE International Journal of Aerospace. 2016, 13 p., 4805817.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
349 Downloads (Pure)

Geometrical Based Method for the Uncertainty Quantification of Correlated Aircraft Loads

Tartaruga, I., Cooper, J., Sartor, P., Lowenberg, M. & Lemmens, Y., 27 Apr 2016, In : Journal of Aeroelasticity and Structural Dynamics. 4, 1, p. 1-20 20 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
118 Downloads (Pure)

Geometrically Nonlinear Aeroelastic Stability Analysis and Wind Tunnel Test Validation of a Very Flexible Wing

Xie, C., Liu, Y., Yang, C. & Cooper, J., 4 May 2016, In : Journal of Shock and Vibration. 2016, 17 p., 5090719.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
12 Citations (Scopus)
287 Downloads (Pure)

Interpretation of Bending/Torsion Coupling for Swept, Nonhomogenous Wings

Stodieck, O. A., Cooper, J. E. & Weaver, P. M., Jul 2016, In : Journal of Aircraft. 53, 4, p. 892-899 8 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
6 Citations (Scopus)
549 Downloads (Pure)

Nonlinear Folding Wing-Tips for Gust Loads Alleviation

Castrichini, A., Hodigere Siddaramaiah, V., Calderon, D., Cooper, J., Wilson, T. & Lemmens, Y., 17 Feb 2016, In : Journal of Aircraft. 53

Research output: Contribution to journalArticle (Academic Journal)

29 Citations (Scopus)

Parametric reduced order model approach for rapid dynamic loads prediction

Castellani, M., Lemmens, Y. & Cooper, J. E., May 2016, In : Aerospace Science and Technology. 52, p. 29-40 12 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
7 Citations (Scopus)
267 Downloads (Pure)
Open Access
File
6 Citations (Scopus)
419 Downloads (Pure)

Prediction and uncertainty propagation of correlated time-varying quantities using surrogate models

Tartaruga, I., Cooper, J., Lowenberg, M. H., Sartor, P. N., Coggon, S. & Lemmens, Y., 1 Mar 2016, In : CEAS Aeronautical Journal. 7, 1, p. 29-42 14 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
10 Citations (Scopus)
209 Downloads (Pure)
2015

Design of a Morphing Wing tip

Cooper, J., Chekkal, I., Cheung, R., Wales, C., Allen, N., lawson, S., Peace, A., Cook, R., Standen, P., Hancock, S. & Carossa, G., Sep 2015, In : Journal of Aircraft. 52, 5, p. 1394-1403 10 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
15 Citations (Scopus)
262 Downloads (Pure)

Identification of backbone curves of nonlinear systems from resonance decay responses

Londono Monsalve, J., Neild, S. A. & Cooper, J. E., 21 Jul 2015, In : Journal of Sound and Vibration. 348, p. 224-238 15 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
60 Citations (Scopus)
338 Downloads (Pure)

Numerical and Experimental Investigation of Aircraft Panel Deformation During Riveting Process

Abdelal, G., Georgiou, G., Cooper, J. E., Robotham, A., Levers, A. & Lunt, P., Feb 2015, In : Journal of Manufacturing Science and Engineering. 137

Research output: Contribution to journalArticle (Academic Journal)

18 Citations (Scopus)

Optimization of Tow-Steered Composite Wing Laminates for Aeroelastic Tailoring

Stodieck, O., Cooper, J. E., Weaver, P. M. & Kealy, P., Aug 2015, In : AIAA Journal. 53, 8, p. 2203-2215 13 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
32 Citations (Scopus)
607 Downloads (Pure)

Reduced Order Model Approach for Efficient Aircraft Loads Prediction

Castellani, M., Lemmens, Y. & Cooper, J. E., Dec 2015, In : SAE International Journal of Aerospace. 8, 2, p. 273-281 9 p.

Research output: Contribution to journalArticle (Academic Journal)

Open Access
File
1 Citation (Scopus)
305 Downloads (Pure)
2014

Aeroelastic tailoring and scaling using Bacterial Foraging Optimisation

Georgiou, G., Vio, GA. & Cooper, J. E., Jul 2014, In : Structural and Multidisciplinary Optimization. 50, 1, p. 81-99 19 p.

Research output: Contribution to journalArticle (Academic Journal)

11 Citations (Scopus)

Feedback Linearisation for Nonlinear Vibration Problems

Jiffri, S., Paoletti, P., Cooper, J. E. & Mottershead, J., 5 Jun 2014, In : Journal of Shock and Vibration. 16 p., 106531.

Research output: Contribution to journalArticle (Academic Journal)

9 Citations (Scopus)

Rapid Prediction of Worst Case Gust Loads Following Structural Modification

Khodaparast, HH. & Cooper, J. E., Feb 2014, In : AIAA Journal. 52, 2, p. 242-254

Research output: Contribution to journalArticle (Academic Journal)

22 Citations (Scopus)

Receptance-Based Active Aeroelastic Control Using Multiple Control Surfaces

Singh, K., McDonough, L., Kolonay, R. & Cooper, J. E., Jan 2014, In : Journal of Aircraft. 51, 1, p. 335-341 7 p.

Research output: Contribution to journalArticle (Academic Journal)

29 Citations (Scopus)

Uncertainty quantification of aeroelastic stability of composite plate wings using lamination parameters

Scarth, C., Cooper, J. E., Weaver, P. M. & Silva, G. H. C., 1 Jan 2014, In : Composite Structures. 116, 1, p. 84-93 10 p.

Research output: Contribution to journalArticle (Academic Journal)

41 Citations (Scopus)