Simplifying simulation
Robert Roe investigates the use of simulation within
the aerospace industry and the steps taken to reduce the complexity of software for engineers
soſtware vendors to create packages that can take more of the work off the users by streamlining or even automating processes. Soſtware that is easier to use allows engineers
A
more time to focus on simulation and analysis of the data rather than trying to adapt to new soſtware, learn proprietary coding languages, or the worrying about how to map algorithms to the latest GPU or accelerator technology. At one level, the move to more user-friendly
soſtware can be as straightforward as migrating legacy code from Fortran to newer, more intuitive languages such as Matlab. In complex aerospace design problems, on the other hand, sophisticated soſtware that can automate much of the process of optimising designs can shorten development times and make design engineers more productive. Sometimes, the benefits in aerospace engineering come not solely from the soſtware alone but by coupling the package to novel manufacturing techniques such as 3D printing. Aircraſt noise has become a major concern
and in some cases is an obstacle to growth in air transport as numbers of airports place restrictions on the amount of noise that can be generated by an aircraſt. Designers and engineers must work hard to reduce the noise of jet engines by placing acoustic
32 SCIENTIFIC COMPUTING WORLD
t all stages of aerospace design, engineers find themselves using models of increasing complexity. In turn, this generates a requirement on
Airbus: Nacelle liner acoustic simulation
liners in the nacelle, a housing that holds engines, fuel, or equipment on an aircraſt, to minimise the fan noise radiated from the engine. One example of the use of MSC soſtware
for acoustic simulation looked at the use of nacelle liners on Airbus aircraſt. Te company evaluated several different shapes and materials to understand the best performance. Airbus found that it could dramatically reduce
the time required to design and evaluate acoustic liners by moving to a simulation-based process using Actran acoustic simulation soſtware developed by Free Field Technologies (FFT), a subsidiary of MSC. Diego Copiello, MSC product marketing
manager and senior application engineer, said: ‘Liners are absolutely fundamental to the aircraſt design. If you want to reduce the noise generated by the engine, the only technology that you can apply in the nacelle is to use the liners.’ Te design of the nacelle itself is made more
difficult by several factors, first of which is that the final geometry of the nacelle may not yet be finalised, so any design may have to accommodate changes in the shape of the nacelle in which it is housed. Another restraint is the materials that can be
used for the nacelle liner, as Copiello explained: ‘You cannot use a porous material on a nacelle for
secures soaring success
example, because porous materials absorb and keep the water or kerosene so there is a risk of ice formation or there is a fire hazard.’ Copiello went on to highlight how this restricts
the potential design options available to engineers looking to optimise the design of these liners for commercial aircraſt, as they have no choice but to innovate when designing the geometry of the liner to allow for the greatest increase in performance. Even a small part of an aircraſt, which at first
glance may seem insignificant, oſten requires several simulations and a delicate balance must be struck between performance, cost and weight. Another oſten overlooked layer of complexity is in the combination of different disciplines or different types of data that need to be integrated to provide a clear picture of the overall behaviour of the system. Tis could take the form of FEA, CFD, or thermal analysis as well as acoustic. To combat increasing complexity, soſtware
developers abstract complexity or completely automate features that traditionally would have required many man-hours’ work in repeating experiments or simulations. In the case of Airbus, the engineers found they could automate the optimisation process when designing the nacelle liners. Copiello said: ‘So the automated liner
optimisation chain basically gives Airbus the possibility to run everything automatically.’ Te team at Airbus developed an integrated
numerical chain for Actran in order to streamline its use by acoustics engineers who are not numerical experts. Te chain, called the Automated Liner Optimization Chain for Nacelles Air Inlets and Exhausts (ANaNax), automated the simulation process from engine geometry to results. A typical optimisation loop for the nacelle
liner requires evaluation of 80 liner iterations and three flight conditions at a frequency range from 125Hz to 5650Hz, which means several thousand different iterations.
@scwmagazine l
www.scientific-computing.com
MSC Software
Page 1 |
Page 2 |
Page 3 |
Page 4 |
Page 5 |
Page 6 |
Page 7 |
Page 8 |
Page 9 |
Page 10 |
Page 11 |
Page 12 |
Page 13 |
Page 14 |
Page 15 |
Page 16 |
Page 17 |
Page 18 |
Page 19 |
Page 20 |
Page 21 |
Page 22 |
Page 23 |
Page 24 |
Page 25 |
Page 26 |
Page 27 |
Page 28 |
Page 29 |
Page 30 |
Page 31 |
Page 32 |
Page 33 |
Page 34 |
Page 35 |
Page 36 |
Page 37 |
Page 38 |
Page 39 |
Page 40