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Preview of the 75th Anniversary of aerospace engineering at the University of Bristol online collection

Published online by Cambridge University Press:  09 January 2023

Jonathan E Cooper*
Affiliation:
RAEng Airbus Sir George White Professor of Aerospace Engineering University of Bristol
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Abstract

Type
Other
Copyright
© The Author(s), 2023. Published by Cambridge University Press on behalf of Royal Aeronautical Society

This online collection commemorates 75 years of aerospace engineering teaching and research at the University of Bristol. However, interactions with the aircraft industry started long before the Department was formed in 1946 [Reference Aplin1], for instance when in 1918 the University began teaching a class in Aircraft Manufacturing. An early graduate of University of Bristol Engineering was Leslie Frise, who was hired by the Bristol Aeroplane Company to assist Chief Designer Frank Barnwell. Among accomplishments in his career, Frise designed the Type 156 Bristol Beaufighter, the Bristol Fighter in 1916 and the Bulldog in 1927. His most lasting contribution was the invention of the Frise Aileron, popular on many older aircraft, such as the Piper Cub, a major pre-WWII trainer in the USA. Frise took over as Chief Designer from Barnwell in 1936 and then became Chief Engineer after Barnwell’s death. Another significant graduate from the pre-department years was Archibald Russell. He was appointed Chief Designer of Bristol Aeroplane Company in 1946, becoming a leading structures expert and, eventually, Managing Director and then Chairman at British Aircraft Corporation Filton.

In June 1945, at the end of the second world war, the Bristol Aeroplane Company offered to fund a Chair in Aeronautical Engineering at the University [Reference Severn2]. Sir Alfred Pugsley, who had been the distinguished Head of Structural Engineering at the Royal Aircraft Establishment (RAE) Farnborough had just taken up the chair of Civil Engineering at Bristol. He persuaded Roderick Collar, a mathematician and engineer with whom he had worked closely with at the RAE during the war, to apply and he was appointed as the first holder of the Sir George White Chair [Reference Severn2]. The first six undergraduates arrived in October 1946 and graduated in 1948.

Fast forwarding to the present day, the Aerospace Engineering Department has grown to around 650 undergraduates, 250 PhD students and 40 MSc students, 60 post-doctoral researchers and 50 academic staff. It is one of the leading worldwide providers of aerospace engineering university education combined with blue sky and applied research, with excellent experimental facilities complementing computational modelling expertise. The most notable areas of research expertise are in aerodynamics, aeroacoustics, aeroelasticity, composites, dynamics, flight mechanics and flight sciences.

This special online edition contains a series of papers published during the past year in The Aeronautical Journal by members of the Department of Aerospace Engineering, and also a selection of papers taken from the 75 years since its formation.

Since the earliest days of the department, aerodynamics has always been a key strength, with work focussing upon improving the computational modelling of critical aerodynamic phenomena. The recent paper A Frequency Domain Approach for Reduced Order Transonic Modelling [Reference Gaitonde, Jones and Cooper3] describes an efficient method for the construction of an approximately balanced aerodynamic reduced order model (ROM) via the frequency domain using computational fluid dynamics data. The ROMs produced with this approach, using a small number of frequency simulations, are demonstrated using the system response for inviscid flow about an NLR7301 aerofoil and the FFAST wing, and viscous flow about the NASA Common Research Model. It is shown how the resulting models agree very well with time domain computations but with a significantly reduced computational effort.

Other papers focussed upon aerodynamics include studies on a 2D space time method for unsteady flows including geometric and topological changes [Reference Ederra4], compressible laminar boundary layers [Reference Crabtree5], the development of a cell-vertex upwind scheme for two-dimensional supersonic Euler flows [Reference Allen and Fiddes6], the modelling of the vortex lift of rotating samara seeds [Reference Rezgui, Arroyo and Theunissen7], and the use of pulse responses for the system reduction of 2D unsteady flows generated using CFD [Reference Gaitonde and Jones8].

The founder of the Department, Prof A R Collar, had a renowned expertise in aeroelasticity and developed the well-known ‘aeroelastic triangle’. Several of his papers outline developments in the field, including the George Taylor Gold Medal paper in 19479 and the second Lanchester Lecture [10]. A focus on aeroelasticity has continued to be a constant theme throughout the past 75 years, for instance, Simpson [Reference Simpson11] described an approach for flutter calculations on a desktop computer (using no more than 512k of memory). More recently, RAeS written paper prizes were awarded for work describing the benefits, in terms of improved flight performance, of using floating folding wing-tips for gust loads alleviation [Reference Castrichini, Siddaramaiah, Wilson and Lemmens12] and the development of aeroservoelastic designs for composite wings [Reference Krupa, Cooper, Pirrera and Nangia13].

Aero-acoustics continues to be an important topic and there has been much recent investment in acoustic wind tunnels at Bristol. Martin Lowson, a former head of department and Sir George White Chair holder, was award the Busk prize for a paper describing progress towards the development of quieter civil helicopters [Reference Lowson14]. A recent paper by Branch et al [15] describes experimental studies measuring unsteady motions and noise from flows around a NACA 16-61 aerofoil.

Aerospace composite structures are another area of significant effort in the Department through the Bristol Composites Institute which has strong links with the National Composites Centre. The paper by Thill et al on morphing skins [Reference Thill, Etches and Bond16] continues to be the most cited paper in The Aeronautical Journal whilst another by Potter et al describes innovative approaches for the manufacture and design of composite structures [Reference Potter, Wisnom, Lowson and Adams17]. Recently, a number of structural model reduction methods have been compared using the test case of a wing-box undergoing large deformations [18].

The final group of papers included in this collection include the development of dynamic gain scheduled control for a Hawk scale model using a pendulum support wind tunnel test rig [Reference Richardson, Lowenberg, Jones and Dubs19], the control of UAV perched landings [20] and the measurement of landing gear ground manoeuvre statistics using broadcast transponder data [21] (awarded the Young Persons Written paper prize 2021).

References

Aplin, K. et al. 75th Anniversary of Aerospace Engineering at the University of Bristol, accepted for publication in SCITECH 2023.Google Scholar
Severn, R.T., The Development of the Faculty of Engineering in the University of Bristol 1909–2009.Google Scholar
A Frequency Domain Approach for Reduced Order Transonic Aerodynamic Modelling. Gaitonde, A., Jones, D.P. and Cooper, J.E., 2022, 126, pp 14471473.CrossRefGoogle Scholar
Two-dimensional Conservative Spacetime Methods for Unsteady Simulation of Arbitrary Motion, Ederra, F. et al, 2022, 126, pp 17711800.Google Scholar
Crabtree, L. The Compressible Laminar Boundary Layer on a Yawed Infinite Wing. Aeronautical Quarterly, 1954, 5, (2), pp 85100. doi: 10.1017/S0001925900001104.CrossRefGoogle Scholar
Allen, C. and Fiddes, S. A cell-vertex upwind scheme for two-dimensional supersonic Euler flows. The Aeronautical Journal, 1997, 101, (1005), pp 199208. doi: 10.1017/S0001924000066379Google Scholar
Rezgui, D. Arroyo, I.H. and Theunissen, R. Model for sectional leading-edge vortex lift for the prediction of rotating samara seeds performance: The Aeronautical Journal, 2020, 124, (1278), pp 12361261, 1 August 2020.CrossRefGoogle Scholar
Gaitonde, A. and Jones, D. The use of pulse responses and system reduction for 2D unsteady flows using the Euler equations. The Aeronautical Journal, 106, (1063), pp 483492. doi: 10.1017/S0001924000092332.CrossRefGoogle Scholar
Collar, A. The Expanding Domain of Aeroelasticity. The Journal of the Royal Aeronautical Society, 1946, 50, (428), 613636. doi: 10.1017/S0368393100120358 George Taylor Gold Medal 1947.CrossRefGoogle Scholar
The Second Lanchester Memorial Lecture: Aeroelasticity—Retrospect and Prospect Part of: RAeS Lanchester Lecture Papers A. R. Collar, The Aeronautical Journal, 63, (577), January 1959.Google Scholar
Simpson, A. The solution of large flutter problems on small computers, The Aeronautical Journal, 1984, 88, (874), pp 128140. doi: 10.1017/S0001924000020352.Google Scholar
Castrichini, A. Siddaramaiah, V. Hodigere; Calderon, D.E.; Cooper, J.E.; Wilson, T. and Lemmens, Y. Preliminary investigation of use of flexible folding wing tips for static and dynamic load alleviation, The Aeronautical Journal, 2017, 121, (1235), pp 7394, January 1, 2017 RAeS Bronze Medal for Written Paper (2018).Google Scholar
Krupa, E.P. Cooper, J.E.; Pirrera, A. and Nangia, R. Improved aerostructural performance via aeroservoelastic tailoring of a composite wing, The Aeronautical Journal, 2018, 122, (1255), pp 14421474, September 1, 2018 RAeS Gold Medal for Written Paper (2019).CrossRefGoogle Scholar
Lowson, M. Progress towards quieter civil helicopters. The Aeronautical Journal, 1992, 96, (956), pp 209223. doi: 10.1017/S0001924000050508 Busk Prize, 1992.Google Scholar
Steady and unsteady aerodynamic loading of a NACA 16-616 aerofoil in a uniform flow J.A. Branch et al, 2022.Google Scholar
Thill, C., Etches, J., Bond, I,. Potter K and Weaver P. (2008). Morphing Skins. The Aeronautical Journal, 112, (1129), pp 117139. doi: 10.1017/S0001924000003687 Most cited paper in The Aeronautical Journal.CrossRefGoogle Scholar
Potter, K., Wisnom, M., Lowson, M. and Adams, R., Innovative approaches to composite structures. The Aeronautical Journal, 1988, 102, (1012), pp 107111. doi: 10.1017/S0001924000065659Google Scholar
Comparison of Structural Model reduction methods applied to a large deformation wing box, R.R. Medeiros et al, 2021, 125, (1292), pp 16871709.Google Scholar
Richardson, T., Lowenberg, M., Jones, C. and Dubs, A. Dynamic gain scheduled control of a Hawk scale model. The Aeronautical Journal, 2007, 111, (1121), pp 461469. doi: 10.1017/S0001924000004723CrossRefGoogle Scholar
Improvements in Learning to Control Perched Landings, Fletcher, L. et al, 2022, 126, pp 11031123.CrossRefGoogle Scholar
Landing Gear Ground Manoeuvre Statistics from Automatic Dependent Surveillance-Broadcast Transponder Data J. Hoole et al. 2021, 125, (1293), pp 19421976. Young Persons Written Paper Prize 2021.CrossRefGoogle Scholar