Professor Mark Lowenberg
M.Sc.(Eng.)(Witw.), PhD (Bristol)
Expertise
I research nonlinear flight dynamics and control: modeling & simulation, bifurcation analysis and multi-degree-of-freedom wind tunnel testing; these span numerous aerospace dynamics topics. Also environmental impact of aviation.
Current positions
Professor of Flight Dynamics
School of Civil, Aerospace and Design Engineering
Contact
Press and media
Many of our academics speak to the media as experts in their field of research. If you are a journalist, please contact the University’s Media and PR Team:
Research interests
Prof. Lowenberg is a member of the Dept. of Aerospace Engineering and Head of the Dynamics and Control Research Group. His principal research interest is nonlinear flight dynamics in general, including related wind tunnel experimentation, and in the use of bifurcation analysis to study nonlinear systems in particular. This work was instrumental in initiating bifurcation-based flight dynamics studies in the UK, following a number of research contracts with the then Defence Evaluation and Research Agency (DERA). These led DERA to invest in both in-house bifurcation analysis capability and other external contracts aimed at refining the techniques and software for flight dynamics applications. More recently, Lowenberg and his research collaborators have focused not only flight dynamics applications (with Airbus and NASA Langley Research Center) but also aircraft ground manoeuvres and landing gear shimmy analysis (with Airbus) and on periodically forced systems, namely rotor stability (with AgustaWestland Helicopters) and flapping-wing vehicle flight.
The experimental work is presently aimed at the development of a novel wind tunnel multi-degree-of-freedom dynamic test rig for improving the understanding of aircraft behaviour during manoeuvres involving nonlinear/unsteady aerodynamics. The 'manoeuvre rig' allows motions in up to 5DOF under conditions that replicate the onset of departure/upset behaviour, and is designed to be used both to help develop mathematical modelling techniques for such conditions, and to 'physically simulate' responses in a manner as close as possible to free flight. This is a collaborative effort involving Prof M. Goman at De Montfort University and the IIT Kanpur.
Lowenberg has been a member of the AIAA Atmospheric Flight Mechanics Technical Committee (and Technical Co-Chair of the 2012 AIAA Atmospheric Flight Dynamics conference) and previously the AIAA Guidance, Navigation & Control Technical Committee and the Royal Aeronautical Society Aerodynamics Committee. He has served on the EPSRC Peer Review College since 2002. He has co-created (with Prof. Mikhail Goman of De Montfort University/TsAGI) an MSc module/short course on Nonlinear Flight Mechanics.
In addition to research and postgraduate supervision (has or is supervisor/co-supervisor to more than 20 PhD's), Prof. Lowenberg teaches subjects in the 2nd year Flight Mechanics unit, 3rd year Experimental Aerodynamics and the final year Aircraft Dynamics & Control unit in the Masters in Aeronautical Engineering degree programme; and supervises 3rd and 4th year projects, including the final-year Design Project.
Prof. Lowenberg was Senior Tutor and 3rd Year Tutor in the Department during academic year 2012-13, and Head of Department from 2007 to 2011.
Projects and supervisions
Research projects
Applied bifurcation methods for efficient airborne wind energy generation
Principal Investigator
Role
Co-Investigator
Description
Airborne wind energy systems (AWES) are an emerging technology that harvests wind power at higher altitudes than conventional wind turbines do. This is done by tethering an unmanned aerial vehicle…Managing organisational unit
School of Civil, Aerospace and Design EngineeringDates
01/08/2024 to 31/07/2027
Discipline Hopping for Environmental Solutions: Aerospace/Atmospheric Chemistry
Principal Investigator
Role
Co-Principal Investigator
Description
Three-month secondment of Senior RA from Atmospheric Chemistry to Aerospace Engineering in order to facilitate atmospheric modelling for mitigation of non-CO2 emissions on climate impact.Managing organisational unit
Department of Aerospace EngineeringDates
01/01/2022 to 31/03/2022
Mitigation of non-CO2 climate impact of civil aviation - Aerospace Engineering/Atmospheric Chemistry collaboration
Principal Investigator
Role
Co-Principal Investigator
Description
This project connects strong foundations in Aerospace and Atmospheric Chemistry in order to develop tools and recommendations to reduce the impact of non-CO2 emissions from civil aviation on the climate.…Managing organisational unit
Department of Aerospace EngineeringDates
01/10/2020 to 01/04/2024
Experimental Flight Dynamics Testing for Highly Flexible Aircraft
Principal Investigator
Managing organisational unit
Department of Aerospace EngineeringDates
01/09/2020 to 31/08/2023
Experimental Flight Dynamics Testing for Highly Flexible Aircraft
Principal Investigator
Managing organisational unit
School of Civil, Aerospace and Design EngineeringDates
01/09/2020 to 31/08/2023
Thesis supervisions
Development and evaluation of a wind tunnel manoeuvre rig
Supervisors
An investigation into the use of a pendulum support rig for aerodynamic modelling
Supervisors
Investigation into Rotor Blade Stability in Autorotation Using Bifurcation and Continuation Methods
Supervisors
Extending Nonlinear Frequency Analysis to Flight Dynamics and Control Problems
Supervisors
Robust linear and nonlinear modelling and analysis approaches for uncertain aeroelastic systems
Supervisors
Virtual Flight Testing in a Wind Tunnel Using a Manoeuvre Rig
Supervisors
An improved constraint stabilisation technique for Udwadia-Kalaba Formulation
Supervisors
The synergistic incorporation of propulsive and conventional flight control to improve commercial flight safety
Supervisors
Nonlinear Dynamics of High-Aspect-Ratio Wings
Supervisors
Guidance and Control Elements for Improved Access to Space
Supervisors
Publications
Recent publications
01/01/2025Dynamic augmentation of geometrically nonlinear beams via guided axially elastic tendons
Mechanical Systems and Signal Processing
Aeroelastic scaling of a high aspect ratio wing incorporating semi aeroelastic hinge
AIAA SCITECH 2024 Forum
Wind Tunnel Investigations of a Pitch-Free Flexible High Aspect Ratio Aircraft Model
AIAA SciTech Forum and Exposition, 2024
Analysis of inertial gust load relief characteristics of high aspect ratio wings
Aeroelastic Scaling of a High-Aspect-Ratio Wing Incorporating a Semi-Aeroelastic Hinge
AIAA Journal