UOA10-01: Computational fluid dynamics: the Rolls-Royce HYDRA code for jet engine design
Submitting Institution
University of OxfordUnit of Assessment
Mathematical SciencesSummary Impact Type
TechnologicalResearch Subject Area(s)
Mathematical Sciences: Applied Mathematics, Numerical and Computational Mathematics
Information and Computing Sciences: Computation Theory and Mathematics
Summary of the impact
Rolls-Royce uses the HYDRA computational fluid dynamics (CFD) code for
the design of all of its
new gas turbine engines. The HYDRA CFD package, including the mathematical
theory behind it,
was developed by Professor Mike Giles and his research team in the period
1998-2004 at the
University of Oxford, and subsequently transferred to Rolls-Royce, forming
the basis of the RR
corporate CFD strategy with an investment of over 100 person years in
development.
Since 2009, HYDRA has become the standard aerodynamic design tool across
Rolls-Royce, and
has been used to design Rolls-Royce's Trent 1000 engine and the newer
Trent XWB. HYDRA has
enabled Rolls-Royce to save over [text removed for publication] in
test rig expenses, provides
superior accuracy compared to its competitors such as FLUENT, and has
contributed to increases
in engine efficiency of up to [text removed for publication],
which in turn has led to higher sales
and increased revenue for Rolls-Royce.
Underpinning research
In 1993, Professor Mike Giles of the University of Oxford established the
Rolls-Royce University
Technology Centre (UTC) in Computational Fluid Dynamics. Part of the
Numerical Analysis Group,
it was created to investigate and develop mathematical and computational
techniques for use in
the analysis and design of turbo-machinery.
The development of HYDRA, a programme of work at the University of Oxford
running from 1998
to 2004, was led by Professor Mike Giles and was sponsored by Rolls Royce
with supporting
funding from EPSRC. Based on identified Rolls Royce requirements, Giles
set four key goals for
his team: that they should use efficient multi-grid iterative solvers on
complex unstructured grids to
model problems with complex engine geometries; that they should enable the
efficient computation
of linear and nonlinear unsteadiness due to blade flutter and forced
response; that they should use
adjoint design techniques to improve the speed of design optimisation; and
that the whole
computation should execute very efficiently on distributed-memory parallel
clusters.
Turbomachinery flows have hydrodynamic shocks which can be modelled
mathematically as
discontinuities in the flow properties. In prior work, Giles was the first
to show that linear
perturbation methods could be used to analyse the effect of shock
oscillations in inviscid flows.
This was an important background result for the development of HYDRA at
the University of
Oxford, but new research was required to develop efficient multi-grid
solvers for linear unsteady
viscous flows [3].
Giles and his team also developed new adjoint techniques [2,4] to improve
the efficiency of
optimisation calculations. The team moved away from existing adjoint
techniques, instead
developing their own so-called "discrete" approach in which the nonlinear
discretisation is
linearised and then the transposed matrix defines the discrete adjoint
equations. While other
research groups were also working on the subject, HYDRA research pioneered
many of the
developments in the area, including the use of Automatic Differentiation
software to construct
discrete adjoint equations.
Taken as a whole, these advances were combined by Giles' team into a
complete CFD package
called HYDRA which offered:
- use of complex unstructured grids composed of a mix of different
element types, to give
maximum geometric flexibility to handle complex turbomachinery
geometries, including tip
gaps, disk cavities, cooling slots, and internal cooling passages;
- an efficient multigrid solver for time-averaged steady flow
calculation, and for solving the
implicit nonlinear system of equations which comes from approximating
nonlinear unsteady
flow calculations;
- the ability to analyse linearised harmonic unsteady flow perturbations
for both forced
response and flutter analysis;
- an "adjoint" design capability to efficiently compute the sensitivity
of output quantities, such
as engine efficiency, to changes in any one of possibly hundreds of
design variables.
The parallelisation aspects were handled by building on preparatory
research undertaken between
1993 and 1998. This made it possible to hide the parallelism, from both
the HYDRA CFD users
and crucially the HYDRA developers in Oxford, allowing them to concentrate
their efforts on
developing new features within HYDRA [1]. This was a forerunner of modern
high-level abstraction
techniques which are an active research topic today in computer science
addressing the
challenges of many-core computing.
Key researchers from the University of Oxford:
Mike Giles: Reader (1992-1997), Professor (1997-present); Paul Crumpton:
PDRA (1993-1997);
Niles Pierce: PDRA (1997-1998); Mihai Duta: PDRA (2002-2005); Jens Muller:
PDRA (1997-2002)
References to the research
[1] P.I. Crumpton and M.B. Giles. `Multigrid aircraft computations using
the OPlus parallel
library'. pp.339-346 in Parallel Computational Fluid Dynamics:
Implementations and Results
Using Parallel Computers, A. Ecer, J. Periaux, N. Satofuka, and S. Taylor,
editors, North-Holland, 1996. DOI: 10.1.1.48.9819.
Key paper on OPlus parallel framework on which HYDRA is built.
* [2] M.B. Giles, M.C. Duta, J.-D. Muller and N.A. Pierce. `Algorithm
developments for discrete
adjoint methods'. AIAA Journal, 41(2):198-205, 2003. DOI: 10.1.1.10.262.
Key paper, in international journal, on adjoint algorithms in HYDRA;59
Citations (Web of
Science), 108 citations (Google Scholar).
* [3] M.S. Campobasso and M.B. Giles. `Stabilization of a linear flow
solver for turbomachinery
aeroelasticity by means of the recursive projection method', AIAA Journal,
42(9) 1765-1774,
2004. DOI: 10.1007/978-3-540-74460-3_24.
Key paper, in international journal, on linearisation problem; 13
citations (Web of Science),
23 citations (Google Scholar).
* [4] M.B. Giles and NA Pierce. `An introduction to the adjoint approach
to design', Flow,
Turbulence and Combustion, 65(3-4):393-415, 2000. DOI: 10.1.1.135.6053.
Overview paper in international journal; 130 citations (Web of
Science), 280 citations
(Google Scholar).
The three asterisked outputs best indicate the quality of the
underpinning research. All these
papers report research performed exclusively at the University of Oxford.
Details of the impact
The impact is economic: enhanced design capabilities based on the
research have resulted in a
superior product and substantial time and cost savings. The beneficiary is
Rolls-Royce, a world
leader in the design and manufacture of gas turbine engines for aircraft,
ships, power generation
and other applications. Rolls-Royce has been hailed as a star of the
manufacturing sector by the
UK Government, bucking the trend of many of its peers by achieving a total
revenue of over £12.2
bn and record profits of £1.4 bn in 2012 [A], with 85% of its sales abroad
[B] bringing valuable
income to the country, as well as providing employment for almost 20,000
in the UK alone [C].
From research to impact. Rolls-Royce uses CFD codes to simulate
the flow of fluids in and
around all products, including the flow of air through all components of
diesel or gas turbine
engines and their installations [D]. In 2004, Rolls-Royce received from
Oxford the first production
version of the HYDRA CFD code for testing. In 2006 it was established as
the company's
compressor design tool, and by 2009 it had become the design tool for
multiple businesses across
Rolls-Royce — including gas turbines, air and thermal systems, and power
generation [E]. It is one
of the few codes that the company uses for CFD [D].
The many uses of HYDRA within Rolls Royce are illustrated in this
diagram, taken from [F] and
used with permission.
The ability to simulate the flow of air through the engines is crucial to
Rolls-Royce's design
capability, as engines are now designed almost exclusively through
computer simulation with
experimental testing carried out afterwards to verify the performance of
the final design. Rolls-Royce uses HYDRA in various ways: to assess the
aerodynamic efficiency of a design; to assess
the unsteady aerodynamic forces acting on blades due to the passing of
neighbouring blade rows;
to assess the possibility of self-induced vibrations; and to quantify the
heat transfer from the very
hot gases coming out of the combustor into the high pressure turbine
blades [F].
HYDRA offers Rolls-Royce unprecedented accuracy because of its ability to
deal with shocks, and
the company reports that it is now able to rank designs to better than 1%
efficiency, consistently
more impressive than rival packages such as FLUENT. As an example, it
reports that calculated
loss coefficients for industrial exhaust systems now differ from measured
values by just 0.02%,
compared to 0.16% when calculated using FLUENT [E].
Nature and extent of the impact. Of the many impacts of HYDRA to
Rolls-Royce, the greatest
has been on the design of its gas turbine engines for aircraft. The
`soaring demand for more fuel-efficient engines for planes' [G] helped the
civil aerospace arm of the company deliver a 16%
increase in annual revenue to over £6.4 billion in 2012 [A, G] and with
Trent engines, which are
designed using HYDRA, making up around 75% of all orders [A]. Furthermore,
`Rolls-Royce's
order book rose 4% to £60.1bn thanks to strong demand for its Trent
aircraft engines' [B].
HYDRA has given Rolls-Royce a single tool for aerodynamic, aero-acoustic
and aero-elastic
applications. Its novel multi-grid solvers allows the company to
efficiently analyse complex engine
shapes which were previously difficult to assess. Furthermore, the
parallelisation of the software
has cut analysis time, and Rolls-Royce attributes the decrease in design
time for an intermediate
turbine test rig, from [text removed for publication], to the use
of HYDRA's adjoint CFD code [E].
In total, the code has helped save Rolls-Royce at least [text removed
for publication], in test rig
expenses [E]. Rolls-Royce technological development webpage openly credits
HYDRA as one of
the key pieces of technology that make up The Rolls-Royce Engineering
System [D]; for example,
"HYDRA has been used extensively in the design of recent RR products such
as the Trent 1000."
The code was used to design Rolls-Royce's Trent 1000 series of engines,
which power Boeing 787
aeroplanes. By way of illustration of the benefits of improved accuracy
and design capability,
improvements to the latest iteration of the Trent 1000, unveiled in 2012,
over its predecessors
include: [text removed for publication] more efficient
intermediate pressure compressor; [text
removed for publication] more efficient intermediate pressure
turbine; shortened Boeing flight
testbed schedule thanks to design being ahead of time; and a fan assessed
as having "world class
performance" in a Boeing Audit [E]. The Trent 1000 is also the quietest
mode of powering the 787
— some 6 dB quieter than its competitors [C].
The newer Trent XWB, announced in 2007 and then first flown in 2012,
powers the new Airbus
A350 XWB and was also designed using HYDRA. As of May 2012, it was
Rolls-Royce's fastest-selling engine to date, having achieved 1,100 orders
from 34 customers worldwide [C]. Once
again, HYDRA contributed to the improvement of its design, with its high
pressure compressor
seeing an improvement in efficiency of [text removed for publication],
and its intermediate
pressure compressor seeing a [text removed for publication]
improvement, both over the Trent
1000. All told, the Trent XWB is [text removed for publication]
more efficient than the first
generation Trent engines of 1995, making it the most efficient Trent
engine to date.
Sources to corroborate the impact
[A] http://www.rolls-royce.com/investors/financial_reporting/financial_results/index.jsp
[B] http://www.guardian.co.uk/business/2011/nov/11/rolls-royce-engine-recovery-economy
[C] http://www.rolls-royce.com/Images/RR_full_AR_2011_tcm92-34435.pdf
[D] http://www.rolls-royce.com/about/technology/systems_tech/design_systems_tools.jsp
[E] A Brief History of HYDRA, Rolls-Royce internal presentation, supplied
by Chief Design
Systems Architect at Rolls-Royce (who can be contacted), showing the
significance of the
impact of Hydra at Rolls-Royce. Copy held by Oxford University.
[F] Rolls-Royce presentation at ICFD meeting, reading University, 2008,
www.icfd.rdg.ac.uk/ICFD25/Talks/LLapworth.pdf
[G] http://uk.reuters.com/article/2013/02/14/uk-rolls-royce-idUKBRE91D0B720130214?feedType=RSS&feedName=businessNews
[C]-[F] give data about Hydra and its use at Rolls-Royce. [A], [B] &
[G] give evidence of the
economic success of Rolls-Royce engines designed using Hydra.