Dr Branislav Titurus

Search results

• 2024

  Analysis of inertial gust load relief characteristics of high aspect ratio wings

  Jayatilake, S. D., Lowenberg , M. H., Woods, B. K. S. & Titurus, B., Jun 2024.

  Research output: Contribution to conference › Conference Paper

  • High Aspect Ratio 100%
  • Gust Loads 100%
  • Resonant Mode 50%
  • Structural Load 50%
  • Force Transmissibility 50%

• Dynamics of nonlinear beam-propeller system with different numbers of blades

  Wu, J., Rezgui, D. & Titurus, B., 1 Jan 2024, In: Nonlinear Dynamics. 112, 2, p. 833-863 31 p.

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

  Open Access

  • Nonlinear Model 100%
  • Blade Number 100%
  • Propeller 100%
  • Bladed Propeller 66%
  • Rotational Speed 33%

• 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%
  11 Downloads (Pure)

• Experimental Investigation into the Dynamic Characteristics of a Tilting Multirotor System

  Sharma, T., Rezgui, D. & Titurus, B., 2024, International Forum on Aeroelasticity and Structural Dynamics.

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

• 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%

• Systematic Experimental Evaluation of Aeroelastic Characteristics of a Highly Flexible Wing Demonstrator

  Jayatilake, S. D., Lowenberg , M. H., Woods, B. K. S. & Titurus, B., 3 Sept 2024, (E-pub ahead of print) In: AIAA Journal.

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

  Open Access

  File

  • Damping Ratio ζ 100%
  • Flexible Wings 100%
  • Relative Phase 33%
  • Relative Magnitude 33%
  • Flutter Speed 33%
  7 Downloads (Pure)
• 2023

  Analysis of a tendon-based deformation aggregation mechanism to host discrete vibration absorbers in continuum structures

  Jayatilake, S. D., Woods, B. K. S., Lowenberg , M. H. & Titurus, B., Jul 2023.

  Research output: Contribution to conference › Conference Paper

  Open Access

  • Vibration Absorber 100%
  • Degree of Freedom 50%

• 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)

• Identification of varying modal parameters of a tall building from the full-scale wind-induced responses

  Gonzalez-Fernandez, D., De Risi, R., Rezgui, D., Macdonald, J. H. G., Margnelli, A. & Titurus, B., 19 Jul 2023, In: Structures. 56, 104770.

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

  Open Access

  • Full Scale 100%
  • Modal Parameter 100%
  • Tall Buildings 100%
  • Resonant Frequency 100%
  • United Kingdom 100%
  2 Citations (Scopus)

• Model and experimental analysis of a rotor rig dynamics with time-varying characteristics

  Wu, J., Rezgui, D. & Titurus, B., 4 Aug 2023, In: Journal of Sound and Vibration. 557, 117683.

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

  Open Access

  • Rotors 100%
  • Propeller 100%
  • Test Rig 50%
  • Modal Analysis 33%
  • Aircraft 33%
  1 Citation (Scopus)

• Multidomain Synthesis of Optimal Vibration Suppression Systems

  Li, Y., Jiang, J. Z., Neild, S. A. & Titurus, B., 1 Nov 2023, In: Journal of Mechanical Design, ASME. 145, 11, 12 p., 111701.

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

  Open Access

  File

  • Hydraulics 100%
  • Suppression System 100%
  • Realization 50%
  • Performance Improvement 25%
  • Automotives 25%
  44 Downloads (Pure)

• Parametric Studies of Flexible Sandwich Panels As a Compliant Fairing for Folding Wingtip Joints

  Mahid, N., Schenk, M., Titurus, B. & Woods, B. K. S., 27 Nov 2023, ASME 2023 Conference on Smart Materials, Adaptive Structures and Intelligent Systems. American Society of Mechanical Engineers (ASME), 10 p. SMASIS2023-110481. (Proceedings of the ASME Conference on Smart Materials, Adaptive Structures, and Intelligent Systems).

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

  • Joints (Structural Components) 100%
  • Parametric Study 100%
  • Wingtips 100%
  • Sandwich Panel 100%
  • Design Space 66%

• Stability and dynamical analysis of whirl flutter in a gimballed rotor-nacelle system with a smooth nonlinearity

  Mair, C. R. T., Rezgui, D. & Titurus, B., 1 Jul 2023, In: The Aeronautical Journal. 127, 1313, p. 1234 - 1254 21 p.

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

  Open Access

  • Rotors 100%
  • Nonlinearity 100%
  • Flutter Analysis 100%
  • Spectrum Analysis 100%
  • Flaps 14%
  4 Citations (Scopus)
• 2022

  Aeroelastic and gust rejection characteristics of a slender wing suspended by a viscoelastic cord

  Jayatilake, S. D., Lowenberg , M. H., Woods, B. K. S. & Titurus, B., 14 Jun 2022.

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

  • Illustrates 100%
  • Combined System 100%
  • Aerodynamic Load 100%
  • Aeroelastic Tailoring 100%
  • Stability Characteristic 100%

• Aeroelastic characteristics of a rotating blade axially loaded by an internally guided tendon

  Wu, J., Woods, B. K. S. & Titurus, B., 7 Jan 2022, (Unpublished). 15 p.

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

  File

  • Critical Speed 100%
  • Internals 50%
  • Flaps 50%
  • Rotational Speed 50%
  • Rotor Blade 50%
  81 Downloads (Pure)

• Analysis of liquid spring damper for vertical landing reusable launch vehicle with network-based methodology

  Yue, S., Titurus, B., Li, Z., Wu, C. & Du, Z., 8 Oct 2022, In: Nonlinear Dynamics.

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

  Open Access

  File

  • Orifice 100%
  • Reusable Launch Vehicle 100%
  • Launch Vehicle 100%
  • Nonlinear Model 50%
  • Time Domain 25%
  1 Citation (Scopus)

  57 Downloads (Pure)

• Analysis of structural dynamics and damping performance of a beam-tendon system undergoing large shape changes

  Jayatilake, S. D., Woods, B. K. S., Lowenberg , M. H. & Titurus, B., 12 Sept 2022.

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

  • Energy Engineering 100%
  • Structural Damping 100%
  • Beam Structure 100%
  • Prestress 100%
  • Rayleigh-Ritz Method 100%

• 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%
  95 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)

  74 Downloads (Pure)

• Experimental modal analysis of a rotating tendon-loaded helicopter blade demonstrator

  Wu, J., Ondra, V., Luebker, J., Kalow, S., Riemenschneider, J. & Titurus, B., 17 May 2022, (E-pub ahead of print) In: Mechanical Systems and Signal Processing. 178, 109286.

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

  Open Access

  File

  • Axial Load 100%
  • Helicopter Blade 100%
  • Modal Analysis 100%
  • Internals 50%
  • Predicted Result 50%
  5 Citations (Scopus)

  72 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%

• Nonlinear aeroelastic analysis of a damped elastica-aerofoil system

  Jayatilake, S. D. & Titurus, B., 14 May 2022, In: Nonlinear Dynamics. 109, 2, p. 731-754 24 p.

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

  Open Access

  File

  • Structural Model 100%
  • Airfoil 100%
  • Two Dimensional 50%
  • Large Deformation 50%
  • Local Strain 50%
  3 Citations (Scopus)

  76 Downloads (Pure)

• 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)

• 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%

• 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%

• Tendon-inerter-damper helicopter blade augmentation for improved dynamic performance

  Jayatilake, S. D., Wu, J. & Titurus, B., 12 Dec 2022, In: Journal of Sound and Vibration. 547, 29 p., 117509.

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

  Open Access

  • Dynamic Performance 100%
  • Helicopter Blade 100%
  • Parameter Variation 50%
  • Control Parameter 50%
  • Tendon Tension 50%
  3 Citations (Scopus)
• 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)

• Damping augmentation of a rotating beam-tendon system via internally placed spring-damper elements

  Wu, J. & Titurus, B., 3 Jul 2021, In: Journal of Sound and Vibration. 510, 25 p., 116315.

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

  Open Access

  File

  • Damping Ratio ζ 100%
  • Rotating Beam 100%
  • Axial Force 75%
  • Energy Engineering 25%
  • Damping Property 25%
  11 Citations (Scopus)

  41 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)

• Free vibration and stability analysis of a cantilever beam axially loaded by an intermittently attached tendon

  Ondra, V. & Titurus, B., 1 Sept 2021, In: Mechanical Systems and Signal Processing. 158, 18 p., 107739.

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

  Open Access

  File

  • Free Vibration Analysis 100%
  • Cantilever Beam 100%
  • Stability Analysis 100%
  • Boundary Value 33%
  • Axial Load 33%
  15 Citations (Scopus)

  65 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)

• Modal analysis of a rotating pre-twisted beam axially loaded by an internally guided tendon

  Wu, J. & Titurus, B., 28 Apr 2021, In: Journal of Sound and Vibration. 498, 23 p., 115980.

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

  Open Access

  File

  • Axial Force 100%
  • Modal Analysis 100%
  • Resonant Frequency 100%
  • Energy Engineering 33%
  • Mode Shape 33%
  11 Citations (Scopus)

  81 Downloads (Pure)

• Modal characterisation of a rotor/propeller rig for tip-mach scaled wind tunnel testing

  Tatar, A., Wu, J., Zagaglia, D., Titurus, B., Rezgui, D., Green, R. & Barakos, G., 8 Sept 2021. 10 p.

  Research output: Contribution to conference › Conference Paper

  Open Access

  File

  • Rotors 100%
  • Propeller 100%
  • Finite Element Methods 50%
  • Modal Testing 50%
  • Shaft 50%
  73 Downloads (Pure)

• 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)

  55 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)

• Stability analysis of whirl flutter in rotor-nacelle systems with freeplay nonlinearity

  Mair, C., Titurus, B. & Rezgui, D., 27 Feb 2021, In: Nonlinear Dynamics. 2021, 25 p.

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

  Open Access

  File

  • Rotors 100%
  • Stability Analysis 100%
  • Nonlinearity 100%
  • Linear Analysis 33%
  • Degree of Freedom 16%
  18 Citations (Scopus)

  203 Downloads (Pure)

• Vibration control of a rotating Timoshenko beam-tendon system via internal guiding inerter-dampers

  Wu, J. & Titurus, B., 5 Nov 2021, In: Journal of Sound and Vibration. 516, 23 p., 116542.

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

  Open Access

  File

  • Internals 100%
  • Axial Force 100%
  • Vibration Control 100%
  • Damping Ratio ζ 50%
  • Damping Coefficient 50%
  9 Citations (Scopus)

  29 Downloads (Pure)
• 2020

  Experimental identification of whirl flutter characteristics in a small-scale rotor rig

  Tatar, A., Rezgui, D. & Titurus, B., 9 Sept 2020, Proceedings of ISMA2020. Heverlee (Belgium): KU Leuven, p. 231-246 16 p.

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

  Open Access

  File

  • Rotors 100%
  • Test Rig 20%
  • Transients 20%
  • Geometric Nonlinearity 20%
  • Scale Experiment 20%
  337 Downloads (Pure)

• Numerical and experimental modal analysis of a cantilever beam axially loaded by a tendon which is attached in a single spanwise location

  Ondra, V. & Titurus, B., 1 Jan 2020, (E-pub ahead of print) Topics in Modal Analysis and Testing, Volume 8 - Proceedings of the 37th IMAC, A Conference and Exposition on Structural Dynamics 2019: Proceedings of the 37th IMAC, A Conference and Exposition on Structural Dynamics 2019. Mains, M. L. & Dilworth, B. J. (eds.). Springer New York LLC, p. 107-116 10 p. (Conference Proceedings of the Society for Experimental Mechanics Series).

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

  • Modal Analysis 100%
  • Rotorcraft 100%
  • Cantilever Beam 100%
  • Rotary Wing Aircraft 100%
  • Modal Testing 100%
  8 Citations (Scopus)

• Polynomial Nonlinear State Space Identification of an Aero-Engine Structure

  Cooper, S. B., Tiels, K., Titurus, B. & Di Maio, D., 1 Oct 2020, In: Computers and Structures. 238, 20 p., 106299.

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

  Open Access

  File

  • Joints (Structural Components) 100%
  • Aero-Engines 100%
  • Measured Data 50%
  • Nonlinear Function 50%
  • Frequency Domain 50%
  7 Citations (Scopus)

  112 Downloads (Pure)

• Sloshing fluid-structure interaction and induced damping effects: modelling and experimental analysis

  Constantin, L., De Courcy, J., Titurus, B., Rendall, T. C. S. & Cooper, J. E., 7 Sept 2020, Proceedings of ISMA2020 International Conference on Noise and Vibration Engineering. p. 859-872 14 p.

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

  • Transient Analysis 100%
  • Experimental Measurement 100%
  • Damping Effect 100%
  • Fluid-Structure Interaction 100%
  • Degree of Freedom 50%
  3 Citations (Scopus)
• 2019

  Aeroelastic eigenvalue analysis of a variable speed rotor blade with an applied compressive load

  Dibble, R., Ondra, V., Woods, B. K. S. & Titurus, B., 6 Jan 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc. (AIAA), (AIAA Scitech 2019 Forum).

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

  Open Access

  File

  • Rotor Blade 100%
  • Eigenvalue Analysis 100%
  • Compression Load 100%
  • Variable Speed Rotor 100%
  • Rotor Speed 100%
  5 Citations (Scopus)

  296 Downloads (Pure)

• An active tendon concept in rotorcraft with variable speed rotors: free vibration perspective: Free vibration perspective

  Ondra, V., Dibble, R. P., Titurus, B. & Woods, B. K. S., 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc. (AIAA), (AIAA Scitech 2019 Forum).

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

  • Rotorcraft 100%
  • Variable Speed Rotor 100%
  • Free Vibration 100%
  • Rotor Blade 75%
  • Main Rotor 75%
  11 Citations (Scopus)

• Free vibration analysis of a rotating pre-twisted beam subjected to tendon-induced axial loading

  Ondra, V. & Titurus, B., 24 Nov 2019, In: Journal of Sound and Vibration. 461, 19 p., 114912.

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

  Open Access

  File

  • Axial Loading 100%
  • Rotation Speed 100%
  • Free Vibration Analysis 100%
  • Free Vibration 100%
  • Resonant Frequency 100%
  20 Citations (Scopus)

  101 Downloads (Pure)

• Generalisable model development for fluid-inerter integrated damping devices

  Liu, X., Titurus, B. & Jiang, J. Z., 1 Jul 2019, In: Mechanism and Machine Theory. 137, p. 1-22 22 p.

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

  • Design Parameter 100%
  • Similarities 33%
  • Hydraulics 33%
  • Vibration Absorber 33%
  • Network Element 33%
  21 Citations (Scopus)

• Liquid spring damper for vertical landing Reusable Launch Vehicle under impact conditions

  Yue, S., Titurus, B., Nie, H. & Zhang, M., 15 Apr 2019, In: Mechanical Systems and Signal Processing. 121, p. 579-599 21 p.

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

  Open Access

  File

  • Impact Condition 100%
  • Reusable Launch Vehicle 100%
  • Degree of Freedom 25%
  • Good Match 25%
  • Test Result 25%
  17 Citations (Scopus)

  598 Downloads (Pure)

• Passive Gust Loads Alleviation in a Truss-Braced Wing Using an Inerter-Based Device

  Szczyglowski, C. P., Neild, S. A., Titurus, B., Jiang, J. Z. & Coetzee, E., 2019, In: Journal of Aircraft. 12 p.

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

  Open Access

  File

  • Gust Loads 100%
  • Aerospace Applications 50%
  • Damping Coefficient 50%
  • Peak Load 50%
  9 Citations (Scopus)

  389 Downloads (Pure)

• Resonance avoidance for variable speed rotor blades using an applied compressive load

  Dibble, R., Ondra, V. & Titurus, B., 1 May 2019, In: Aerospace Science and Technology. 88, p. 222-232 11 p.

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

  Open Access

  File

  • Rotor Blade 100%
  • Compression Load 100%
  • Variable Speed Rotor 100%
  • Rotor Speed 66%
  • Resonant Frequency 66%
  21 Citations (Scopus)

  167 Downloads (Pure)

• Stability Analysis of Whirl Flutter in a Nonlinear Gimballed Rotor-Nacelle System

  Mair, C., Rezgui, D. & Titurus, B., 7 Jun 2019, Proceedings of the 75th Forum of the Vertical Flight Society. Philadelphia, Pennsylvania: Vertical Flight Society, p. 1-16 16 p. 389. (Annual Forum Proceedings; vol. 75).

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

  File

  • Rotors 100%
  • Stability Analysis 100%
  • Nonlinearity 100%
  • Linear Analysis 33%
  • Rotor Blade 33%
  414 Downloads (Pure)