Professor Jonathan E Cooper

Search results

• 2024

  Aeroelastic Scaling of a High-Aspect-Ratio Wing Incorporating a Semi-Aeroelastic Hinge

  Gu, H., Healy, F. J., Constantin, L., Rezgui, D., Lowenberg, M. H., Cooper, J. E., Wilson, T. & Castrichini, A., 16 Apr 2024, In: AIAA Journal. 13 p.

  Research output: Contribution to journal › Article (Academic Journal) › peer-review

  Open Access

  File

  • Iso 100%
  • High Aspect Ratio 100%
  • Wingtips 75%
  • Full Scale 25%
  • Aeroelastic Behavior 25%
  38 Downloads (Pure)

• Aeroelastic scaling of a high aspect ratio wing incorporating semi aeroelastic hinge

  Gu, H., Healy, F. J., Rezgui, D., Lowenberg, M. H. & Cooper, J. E., 4 Jan 2024, AIAA SCITECH 2024 Forum. American Institute of Aeronautics and Astronautics Inc. (AIAA), 2024-0618

  Research output: Chapter in Book/Report/Conference proceeding › Conference Contribution (Conference Proceeding)

  Open Access

  File

  • Iso 100%
  • Wingtips 100%
  • High Aspect Ratio 100%
  • Good Agreement 33%
  • Full Scale 33%
  46 Downloads (Pure)

• Experimental analysis of liquid vertical slosh damping at vacuum and atmospheric pressures

  Constantin, L., Titurus, B., Rendall, T. C. S., De Courcy, J. J. & Cooper, J. E., 31 Mar 2024, In: Journal of Sound and Vibration. 574, 118228.

  Research output: Contribution to journal › Article (Academic Journal) › peer-review

  Open Access

  File

  • Atmospheric Pressure 100%
  • Aerodynamic Damping 50%
  • Liquid Gas 50%
  • Aerodynamic Effect 50%
  • Density Ratio 50%
  8 Downloads (Pure)

• Experimental and Numerical Nonlinear Stability Analysis of Wings Incorporating Flared Folding Wingtips

  Healy, F. J., Cheung, R. C. M., Rezgui, D., Cooper, J. E., Wilson, T. & Castrichini, A., 1 Jan 2024, In: Journal of Aircraft. 61, 1, p. 140-154 15 p.

  Research output: Contribution to journal › Article (Academic Journal) › peer-review

  Open Access

  File

  • Wingtips 100%
  • Stability Analysis 100%
  • Stability Boundary 57%
  • Dynamic Behavior 14%
  • Bifurcation Analysis 14%
  93 Downloads (Pure)

• Flight dynamics of aircraft incorporating the semi-aeroelastic hinge

  Gu, H., Healy, F., Jayatilake, S., Rezgui, D., Lowenberg, M., Cooper, J., Wilson, T. & Castrichini, A., 1 Apr 2024, In: Aerospace Science and Technology. 147, 14 p., 109026.

  Research output: Contribution to journal › Article (Academic Journal) › peer-review

  Open Access

  • Wingtips 100%
  • Flight Dynamics 100%
  • Release Time 33%
  • Gust Loads 33%
  • Transient Analysis 16%
  2 Citations (Scopus)

• Incompressible δ-SPH via artificial compressibility

  De Courcy, J. J., Rendall, T. C. S., Constantin, L., Titurus, B. & Cooper, J. E., 15 Feb 2024, In: Computer Methods in Applied Mechanics and Engineering. 420, 40 p., 116700.

  Research output: Contribution to journal › Article (Academic Journal) › peer-review

  Open Access

  • Time Integration 100%
  • Time Step 100%
  • Residuals 100%
  • Lagrangian 100%
  • Incompressible Flow 100%

• Nonlinear Stability Analysis of Floating Wingtips with Control Surface Freeplay

  Healy, F. J., Gu, H., Rezgui, D. & Cooper, J. E., 4 Jan 2024, AIAA SCITECH 2024 Forum. American Institute of Aeronautics and Astronautics Inc. (AIAA), 2024-1267

  Research output: Chapter in Book/Report/Conference proceeding › Conference Contribution (Conference Proceeding)

  Open Access

  File

  • Wingtips 100%
  • Control Surfaces 100%
  • Stability Analysis 100%
  • Flutter Speed 25%
  • Airframe 25%
  14 Downloads (Pure)
• 2023

  Experimental Effect of Liquid Sloshing on the Dynamic Behaviour of Flared Folding Wingtips

  Healy, F. J., De Courcy, J. J., Gu, H., Rezgui, D. & Cooper, J. E., 19 Jan 2023, AIAA SCITECH 2023 Forum. American Institute of Aeronautics and Astronautics Inc. (AIAA), 2023-2569

  Research output: Chapter in Book/Report/Conference proceeding › Conference Contribution (Conference Proceeding)

  • Dynamic Behavior 100%
  • Wingtips 100%
  • Angle-of-Attack 12%
  • Aeroelastic Behavior 12%
  • Negligible Effect 12%

• Experimental Effect of Sideslip Angle on the Dynamic Behaviour of Flared Folding Wingtips

  Healy, F. J., Rezgui, D. & Cooper, J. E., 27 Jan 2023. 25 p.

  Research output: Contribution to conference › Conference Paper

  Open Access

  File

  • Dynamic Behavior 100%
  • Wingtips 100%
  • Sideslip Angle 100%
  • Flutter Speed 20%
  • Stable Equilibrium 20%
  37 Downloads (Pure)

• Fuel sloshing-induced effects on the dynamic response of a scaled research wing demonstrator

  Constantin, L., De Courcy, J. J., Titurus, B., Rendall, T. C. S. & Cooper, J. E., 1 Sept 2023, In: Aerospace Science and Technology. 140, 108450.

  Research output: Contribution to journal › Article (Academic Journal) › peer-review

  Open Access

  • Wings 100%
  • Dynamic Response 100%
  • Dihedral Angle 50%
  • Energy Dissipation 25%
  • Damping Ratio ζ 25%
  4 Citations (Scopus)

• Low Fidelity Modelling of the Nonlinear Aerodynamics of Spoilers

  Pontillo, A., Banneheka Navaratna, P. D., Lowenberg, M. H., Rezgui, D., Cooper, J. E. & Neild, S. A., 23 Jan 2023, p. 1-18.

  Research output: Contribution to conference › Conference Paper › peer-review

  Open Access

  File

  • Good Agreement 100%
  • Numerical Prediction 100%
  • Load Cell 100%
  • Acquired Data 100%
  • Wingspan 100%
  133 Downloads (Pure)

• Numerical Investigations of Subscale Flexible High Aspect Ratio Aircraft on a Dynamic Wind Tunnel Rig

  Banneheka Navaratna, P. D., Pontillo, A., Rezgui, D., Lowenberg, M. H., Neild, S. A. & Cooper, J. E., 19 Jan 2023, AIAA SCITECH 2023 Forum. American Institute of Aeronautics and Astronautics Inc. (AIAA)

  Research output: Chapter in Book/Report/Conference proceeding › Conference Contribution (Conference Proceeding)

  Open Access

  File

  • Rigid Structure 100%
  • Aircraft Model 100%
  • High Aspect Ratio 100%
  • Internals 50%
  • Degree of Freedom 50%
  5 Citations (Scopus)

  81 Downloads (Pure)

• On the Dynamic Behavior of Wings Incorporating Floating Wingtip Fuel Tanks

  Healy, F., Courcy, J. D., Gu, H., Rezgui, D., Cooper, J., Wilson, T. & Castrichini, A., 7 Nov 2023, (E-pub ahead of print) In: Journal of Aircraft.

  Research output: Contribution to journal › Article (Academic Journal) › peer-review

  Open Access

  File

  • Dynamic Behavior 100%
  • Wingtips 100%
  • Angle-of-Attack 20%
  • Aeroelastic Behavior 20%
  • Fuel Mass 20%
  1 Citation (Scopus)

  36 Downloads (Pure)

• Remote Sensing of Aerospace Usage Profiles via Air Traffic Data

  Hoole, J., Booker, J. D., Cooper, J. E. & Richardson, T. S., 21 Jun 2023, Review of aeronautical fatigue and structural integrity investigations in the UK during the period May 2021 - April 2023. Hallam, D. (ed.).

  Research output: Chapter in Book/Report/Conference proceeding › Chapter in a report

  Open Access

• Sizing of High-Aspect-Ratio Wings with Folding Wingtips

  Gu, H., Healy, F. J., Rezgui, D. & Cooper, J. E., 1 Mar 2023, In: Journal of Aircraft. 60, 2, p. 461-475 15 p.

  Research output: Contribution to journal › Article (Academic Journal) › peer-review

  Open Access

  File

  • Wingtips 100%
  • High Aspect Ratio 100%
  • Design Process 33%
  • Aerodynamic Load 33%
  • Wingspan 33%
  10 Citations (Scopus)

  280 Downloads (Pure)

• Transient Release and Lateral Gust Behavior of Aircraft Incorporating Flared Folding Wingtips

  Gu, H., Cheung, R. C., Healy, F., Goodarzi Ardakani, V., Abdo, S., Rezgui, D., Lowenberg, M. H. & Cooper, J. E., 19 Jan 2023, AIAA SCITECH 2023 Forum. p. 2568 1 p.

  Research output: Chapter in Book/Report/Conference proceeding › Conference Contribution (Conference Proceeding)
• 2022

  Aeroelastic tailoring optimisation of a combat aircraft wing with tow-steered composites

  Tatar, A., Cheung, R. C. M., Cooper, J. E., Pearson, D. P. & Warsop, C., 13 Jun 2022.

  Research output: Contribution to conference › Conference Paper

  Open Access

  File

  • Wings 100%
  • Aeroelastic Tailoring 100%
  • Combat Aircraft 100%
  • Structural Constraint 66%
  • Aeroelastic Behavior 33%
  57 Downloads (Pure)

• A frequency domain approach for reduced- order transonic aerodynamic modelling

  Gaitonde, A. L., Jones, D. P. & Cooper, J. E., 7 Jun 2022, In: The Aeronautical Journal. 126, 27 p.

  Research output: Contribution to journal › Article (Academic Journal) › peer-review

  Open Access

  File

  • Frequency Domain 100%
  • Reduced Order Model 100%
  • Aerodynamic Modeling 100%
  • Time Domain 75%
  • Computational Fluid Dynamics 50%
  85 Downloads (Pure)

• DATA DRIVEN AND MODEL-BASED VERTICAL SLOSHING REDUCED ORDER MODELS FOR AEROELASTIC ANALYSIS

  Saltari, F., De Courcy, J., Pizzoli, M., Constantin, L., Mastroddi ,F., Coppotelli, G., Titurus, B., Rendall, T. C. S., Cooper, J. E. & Gambioli, F., 17 Jun 2022. 19 p.

  Research output: Contribution to conference › Conference Paper › peer-review

  Open Access

  File

  • Reduced Order Model 100%
  • Free Surface 50%
  • Mechanical Model 50%
  • Critical Condition 50%
  • Surrogate Model 50%
  92 Downloads (Pure)

• Effect of Fuel Sloshing on the Damping of a Scaled Wing Model – Experimental Testing and Numerical Simulations

  Constantin, L., De Courcy, J., Titurus, B., Rendall, T. C. S., Cooper, J. E. & Gambioli, F., 4 Aug 2022, In: Applied Sciences. 12, 15, 24 p., 7860.

  Research output: Contribution to journal › Article (Academic Journal) › peer-review

  Open Access

  File

  • Experimental Model 100%
  • Computer Simulation 100%
  • Good Agreement 50%
  • Conducted Experiment 50%
  • Damping Effect 50%
  7 Citations (Scopus)

  73 Downloads (Pure)

• Experimental Analysis of the Behaviour of Flared Folding Wingtips with Sideslip Angle

  Healy, F., Cheung, R. C. M., Rezgui, D. & Cooper, J. E., 13 Jun 2022. 17 p.

  Research output: Contribution to conference › Conference Paper

  Open Access

  File

  • Wingtips 100%
  • Sideslip Angle 100%
  • Angle of Incidence 20%
  • Relative Angle 20%
  • Flow Direction 20%
  128 Downloads (Pure)

• Initial Experimental Analysis of Damping due to Liquid Sloshing in a Scaled Aircraft Wing Model

  Constantin, L., De Courcy, J., Titurus, B., Rendall, T. C. S., Cooper, J. E. & Gambioli, F., 17 Jun 2022. 19 p.

  Research output: Contribution to conference › Conference Paper › peer-review

  • Frequency Component 100%
  • Aircraft Wing Model 100%
  • Wings 50%
  • Damping Ratio ζ 50%
  • Multiple Frequency 50%

• LATERAL GUST BEHAVIOUR OF AIRCRAFT INCORPORATING FLARED FOLDING WINGTIPS

  Cheung, R. C. M., Gu, H., Healy, F., Rezgui, D. & Cooper, J. E., 2022, 33rd Congress of the International Council of the Aeronautical Sciences, ICAS 2022. International Council of the Aeronautical Sciences, p. 4113-4127 15 p. (33rd Congress of the International Council of the Aeronautical Sciences, ICAS 2022; vol. 6).

  Research output: Chapter in Book/Report/Conference proceeding › Conference Contribution (Conference Proceeding)

  • Wingtips 100%
  • Flight Mechanics 40%
  • Loading Case 20%
  • Fuel Efficiency 20%
  • Commercial Aircraft 20%
  1 Citation (Scopus)

• Nonlinear damping effects in vertically vibrating systems with violently sloshing liquid

  Constantin, L., De Courcy, J., Titurus, B., Rendall, T. C. S. & Cooper, J. E., 1 Nov 2022, (E-pub ahead of print) In: Journal of Sound and Vibration. 544, 117405.

  Research output: Contribution to journal › Article (Academic Journal) › peer-review

  Open Access
  11 Citations (Scopus)

• Nonlinear Identification of Transient Tank Vertical Sloshing Motions

  Constantin, L., De Courcy, J., Titurus, B., Rendall, T. C. S. & Cooper, J. E., 14 Sept 2022.

  Research output: Contribution to conference › Conference Paper › peer-review

  Open Access

  File

  • Transients 100%
  • Harmonics 50%
  • Wings 25%
  • Excitation Frequency 25%
  • Parametric Study 25%
  62 Downloads (Pure)

• Observations on the Effect of Geometric Nonlinearities on a Representative Civil Aircraft Incorporating Flared Folding Wingtips

  Healy, F., Gu, H., Rezgui, D. & Cooper, J. E., 17 Jun 2022. 19 p.

  Research output: Contribution to conference › Conference Paper

  • Civil Aircraft 100%
  • Wingtips 100%
  • Geometric Nonlinearity 100%
  • Aircraft Structure 33%
  • Dynamic Response 14%

• On the Effect of Geometric Nonlinearity on the Dynamics of Flared Folding Wingtips

  Healy, F., Cheung, R., Rezgui, D., Cooper, J., Wilson, T. & Castrichini, A., 17 Aug 2022, In: Journal of Aircraft. 14 p.

  Research output: Contribution to journal › Article (Academic Journal) › peer-review

  Open Access

  File

  • Wingtips 100%
  • Geometric Nonlinearity 100%
  • Angle-of-Attack 33%
  • Flutter Speed 33%
  • Exact Expression 16%
  8 Citations (Scopus)

  10540 Downloads (Pure)

• Overview of single degree of freedom experiments of vertical sloshing flows inside scaled tanks

  Gonzalez, M. J., Constantin, L., Pizzoli, M., Gonzalez, L., Titurus, B., Cooper, J. E. & Coppotelli, G., 17 Jun 2022. 20 p.

  Research output: Contribution to conference › Conference Paper › peer-review

  • Energy Engineering 100%
  • Degree of Freedom 100%
  • Excitation Frequency 100%
  • Single Degree 100%
  • Transients 100%

• Sizing of High Aspect Ratio Wings with Folding Wingtips

  Gu, H., Healy, F., Rezgui, D. & Cooper, J., 2022, AIAA SciTech Forum 2022. American Institute of Aeronautics and Astronautics Inc. (AIAA), AIAA 2022-0723. (AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022).

  Research output: Chapter in Book/Report/Conference proceeding › Conference Contribution (Conference Proceeding)

  • Wingtips 100%
  • High Aspect Ratio 100%
  • Preliminary Design 33%
  7 Citations (Scopus)

• Statistical analysis of sloshing-induced dissipative energy across a range of Froude numbers

  Constantin, L., De Courcy, J., Titurus, B., Rendall, T. C. S. & Cooper, J. E., Feb 2022.

  Research output: Contribution to conference › Conference Paper › peer-review

  Open Access

  • Energy Engineering 100%
  • Froude Number 100%
  • Liquid Sloshing 100%
  • Energy Dissipation 75%
  • Wings 25%

• Tow-steered Aeroelastic Tailoring for Improved Horizontal Stabiliser Performance

  Cheung, R. C. M., Rezgui, D., Cooper, J. E., Green, R. & Llamas-sandin, R., 27 May 2022, (Accepted/In press) International Forum on Aeroelasticity and Structural Dynamics. Curran Associates, Inc, p. 1838-11855 18 p.

  Research output: Chapter in Book/Report/Conference proceeding › Conference Contribution (Conference Proceeding)

  Open Access

  File

  • Lift-Curve Slope 100%
  • Aeroelastic Tailoring 100%
  • Horizontal Stabilizers 100%
  • Stabilizer 66%
  • Performance Measure ψ 33%
  2 Downloads (Pure)
• 2021

  Analysis of Damping From Vertical Sloshing in a SDOF System

  Constantin, L., De Courcy, J., Titurus, B., Rendall, T. C. S. & Cooper, J. E., 1 May 2021, In: Mechanical Systems and Signal Processing. 152, 24 p., 107452.

  Research output: Contribution to journal › Article (Academic Journal) › peer-review

  Open Access

  File

  • Transients 100%
  • Predictive Capability 66%
  • Model Structure 66%
  • Degree of Freedom 33%
  • Energy Dissipation 33%
  41 Citations (Scopus)

  100 Downloads (Pure)

• Comparison of Structural Model Reduction Methods Applied to a Large-Deformation Wing Box

  Medeiros, R., cesnik, C., Stodieck, O. A., Calderon, D. E., Cooper, J. E. & Coetzee, E., 8 Sept 2021, (E-pub ahead of print) In: The Aeronautical Journal. 125, 1292, p. 1687–1709

  Research output: Contribution to journal › Article (Academic Journal) › peer-review

  Open Access

  File

  • Large Deformation 100%
  • Reduced Order Model 100%
  • Model Reduction 100%
  • Structural Model 100%
  • Beam Model 66%
  5 Citations (Scopus)

  50 Downloads (Pure)

• Design and Assessment of Subscale Flexible High Aspect Ratio Cantilever Wings

  Banneheka Navaratna, P. D., Pontillo, A., Rezgui, D., Lowenberg, M. H., Neild, S. A. & Cooper, J. E., 29 Dec 2021, AIAA SciTech Forum 2022: Session: Dynamics of Flexible and Hypersonic Aircraft. American Institute of Aeronautics and Astronautics Inc. (AIAA), 24 p. AIAA-2022-1305. (AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022).

  Research output: Chapter in Book/Report/Conference proceeding › Conference Contribution (Conference Proceeding)

  Open Access

  File

  • Geometric Nonlinearity 100%
  • High Aspect Ratio 100%
  • Mass Distribution 100%
  • Numerical Model 100%
  • Good Agreement 50%
  3 Citations (Scopus)

  134 Downloads (Pure)

• Design and GVT of a dynamically scaled wing structure for fuel sloshing investigations

  Constantin, L., De Courcy, J., Titurus, B., Rendall, T. C. S. & Cooper, J. E., 29 Dec 2021, AIAA SCITECH 2022 Forum. American Institute of Aeronautics and Astronautics Inc. (AIAA), 18 p.

  Research output: Chapter in Book/Report/Conference proceeding › Conference Contribution (Conference Proceeding)

  • Wings 100%
  • Ground Vibration Test 100%
  • Experimental Investigation 50%
  • Mode Shape 50%
  • Scale Dynamic 50%
  6 Citations (Scopus)

• Experimental Aerodynamic Comparison of Active Camber Morphing and Trailing Edge Flaps

  Rivero, A. E., Fournier, S. F. B., Manolesos, M., Cooper, J. E. & Woods, B. K. S., 18 Jan 2021, (Accepted/In press) In: AIAA Journal.

  Research output: Contribution to journal › Article (Academic Journal) › peer-review

  Open Access

  File

  • Flaps 100%
  • Camber Morphing 100%
  • Experimental Aerodynamics 100%
  • Trailing Edge 100%
  • Lift Coefficient 50%
  270 Downloads (Pure)

• Experimental Analysis of the Dynamics of Flared Folding Wingtips via a Novel Tethered Flight Test

  Healy, F., Pontillo, A., Rezgui, D., Cooper, J. E., Kirk, J., Wilson, T. & Castrichini, A., 29 Dec 2021, AIAA SCITECH 2022 Forum: Session: Flexible Aeroelastic Problems of Unmanned Air Vehicles of All Scales. American Institute of Aeronautics and Astronautics Inc. (AIAA), 22 p.

  Research output: Chapter in Book/Report/Conference proceeding › Conference Contribution (Conference Proceeding)

  Open Access

  File

  • Wingtips 100%
  • Flight Test 100%
  • Unmanned Aerial Vehicle 75%
  • Angle-of-Attack 25%
  • Test Method 25%
  13 Citations (Scopus)

  155 Downloads (Pure)

• Folding Wingtips for Improved Roll Performance

  Healy, F., Cheung, R. C. M., Neofet, T., Lowenberg, M. H., Rezgui, D., Cooper, J. E., Castrichini, A. & Wilson, T., 4 Jan 2021, AIAA Scitech 2021 Forum. American Institute of Aeronautics and Astronautics Inc. (AIAA), p. 1-24 24 p. (AIAA Scitech 2021 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference Contribution (Conference Proceeding)

  Open Access

  File

  • Wingtips 100%
  • Wings 40%
  • Aerodynamic Damping 20%
  • Transients 20%
  • Aerodynamic Performance 20%
  19 Citations (Scopus)

  368 Downloads (Pure)

• Folding Wingtips for Improved Roll Performance

  Healy, F., Cheung, R. C. M., Neofet, T., Lowenberg, M. H., Rezgui, D., Cooper, J. E., Castrichini, A. & Wilson, T., 2 Aug 2021, In: Journal of Aircraft.

  Research output: Contribution to journal › Article (Academic Journal) › peer-review

  Open Access

  File

  • Wingtips 100%
  • Wings 40%
  • Aerodynamic Damping 20%
  • Transients 20%
  • Aerodynamic Performance 20%
  19 Citations (Scopus)

  149 Downloads (Pure)

• Gust Loads Alleviation Using Sloshing Fuel

  De Courcy, J., Constantin, L., Titurus, B., Rendall, T. C. S. & Cooper, J. E., 4 Jan 2021, American Institute of Aeronautics and Astronautics Inc. (AIAA): SciTech Forum. p. 1-14 14 p. (AIAA Scitech 2021 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference Contribution (Conference Proceeding)

  • Mechanical Model 100%
  • Structural Damping 100%
  • Simple System 100%
  • Environmental Impact 100%
  • Atmospheric Turbulence 100%
  18 Citations (Scopus)

• Helicopter Flight Manoeuvre Statistics via ADS-B: An Initial Investigation Using the OpenSky Network †

  Hoole, J., Booker, J. D. & Cooper, J. E., 31 Dec 2021, In: Engineering Proceedings. 13, 1, 10 p., 10.

  Research output: Contribution to journal › Article (Academic Journal) › peer-review

  Open Access

  File

  • Spectrum Usage 100%
  • Initial Investigation 100%
  2 Citations (Scopus)

  72 Downloads (Pure)

• Improving Horizontal Stabilizer Performance Using Aeroelastic Tailoring

  Cheung, R. C. M., Rezgui, D., Cooper, J. E., Green, R. & Llamas-sandin, R., 29 Dec 2021, AIAA SCITECH 2022 Forum: Session: Aerodynamic Testing: Ground, Wind-Tunnel and Flight Testing I. American Institute of Aeronautics and Astronautics Inc. (AIAA)

  Research output: Chapter in Book/Report/Conference proceeding › Conference Contribution (Conference Proceeding)

  Open Access

  File

  • Aeroelastic Tailoring 100%
  • Horizontal Stabilizers 100%
  • Stabilizer 100%
  • Aeroelastic Behavior 50%
  • Aerodynamic Load 50%
  4 Citations (Scopus)

  94 Downloads (Pure)

• Landing Gear Ground Manoeuvre Statistics from Automatic Dependent Surveillance-Broadcast Transponder Data

  Hoole, J., Sartor, P. N., Booker, J. D., Cooper, J. E., Gogouvitis, X. V. & Schmidt, R. K., 3 Jun 2021, In: The Aeronautical Journal. 125, 1293, p. 1942-1976 35 p.

  Research output: Contribution to journal › Article (Academic Journal) › peer-review

  • Landing Gear 100%
  • Fatigue Design 20%
  • Cyclic Loads 20%
  • Ground Track 20%
  • Big Data 20%

• Low-order Aeroelastic Modelling of a High Aspect Ratio Wing Aircraft Under Constrained Motion

  Pontillo, A., Banneheka Navaratna, P. D., Ascham, J. H., Lowenberg, M. H., Rezgui, D., Cooper, J. E. & Neild, S. A., 29 Dec 2021, AIAA SciTech Forum 2022: Session: Dynamics of Flexible and Hypersonic Aircraft. American Institute of Aeronautics and Astronautics Inc. (AIAA), 18 p. AIAA 2022-1306. (AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022).

  Research output: Chapter in Book/Report/Conference proceeding › Conference Contribution (Conference Proceeding)

  Open Access

  File

  • Wings 100%
  • Flight Dynamics 100%
  • Flexible Wings 100%
  • Lattice Method 100%
  • Vortex 100%
  4 Citations (Scopus)

  104 Downloads (Pure)

• Nonlinear Stability Analysis and Experimental Exploration of Limit Cycle Oscillations with Flared Folding Wingtips

  Healy, F., Cheung, R. C. M., Rezgui, D. & Cooper, J. E., 29 Dec 2021, AIAA SCITECH 2022 Forum: Session: Flutter and Limit Cycle Oscillation Problems II. American Institute of Aeronautics and Astronautics Inc. (AIAA)

  Research output: Chapter in Book/Report/Conference proceeding › Conference Contribution (Conference Proceeding)

  Open Access

  File

  • Wingtips 100%
  • Experimental Exploration 100%
  • Stability Analysis 100%
  • Limit Cycle 100%
  • Stability Boundary 50%
  5 Citations (Scopus)

  164 Downloads (Pure)

• On the Nonlinear Geometric Behaviour of Flared Folding Wingtips

  Healy, F., Cheung, R. C. M., Rezgui, D., Cooper, J. E., Wilson, T. & Castrichini, A., 29 Dec 2021, AIAA SCITECH 2022 Forum: Session: Flutter and Limit Cycle Oscillation Problems II. American Institute of Aeronautics and Astronautics Inc. (AIAA), 22 p.

  Research output: Chapter in Book/Report/Conference proceeding › Conference Contribution (Conference Proceeding)

  Open Access

  File

  • Wingtips 100%
  • Angle-of-Attack 28%
  • Flutter Speed 28%
  • Geometric Nonlinearity 28%
  • Experimental Result 14%
  13 Citations (Scopus)

  6159 Downloads (Pure)

• Probabilistic Fatigue Methodology for Safe-Life Design and Analysis

  Hoole, J., Sartor, P. N., Booker, J. D., Cooper, J. E., Gogouvitis, X. V., Ghouali, A. & Schmidt, R. K., 30 Jun 2021, Review of aeronautical fatigue and structural integrity investigations in the UK during the period April 2019 - April 2021. Hallam, D. (ed.). p. 2-5

  Research output: Chapter in Book/Report/Conference proceeding › Chapter in a report

• Sloshing induced damping across Froude numbers in a harmonically vertically excited system

  Constantin, L., De Courcy, J., Titurus, B., Rendall, T. C. S. & Cooper, J. E., 13 Oct 2021, In: Journal of Sound and Vibration. 510, 25 p., 116302.

  Research output: Contribution to journal › Article (Academic Journal) › peer-review

  Open Access

  File

  • Froude Number 100%
  • Harmonics 100%
  • Metrics 50%
  • Rectangular Tank 50%
  • Flow Regime 50%
  22 Citations (Scopus)

  54 Downloads (Pure)

• Sloshing induced damping in vertically vibrating systems

  De Courcy, J., Constantin, L., Titurus, B., Rendall, T. C. S. & Cooper, J. E., 22 Jan 2021, IOP Conference Series: Materials Science and Engineering. 1 ed. Vol. 1024. (IOP Conference Series: Materials Science and Engineering).

  Research output: Chapter in Book/Report/Conference proceeding › Conference Contribution (Conference Proceeding)

  Open Access

  • Free Surface 100%
  • Wings 50%
  • Good Agreement 50%
  • Degree of Freedom 50%
  • Transient Analysis 50%
  4 Citations (Scopus)
• 2020

  Aeroelastic stability analysis of aircraft wings with initial curvature

  Amoozgar, M., Fazelzadeh, S., khodarapast, H., Friswell, M. & Cooper, J. E., 1 Dec 2020, In: Aerospace Science and Technology. 107, 10 p., 106241.

  Research output: Contribution to journal › Article (Academic Journal) › peer-review

  Open Access

  File

  • Wings 100%
  • Initial Curvature 100%
  • Stability Analysis 100%
  • Projected Area 66%
  • Aerodynamic Model 33%
  17 Citations (Scopus)

  63 Downloads (Pure)