Proceedings of the 2001 ACM/IEEE Conference on Supercomputing 2001
DOI: 10.1145/582034.582059
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An automatic design optimization tool and its application to computational fluid dynamics

Abstract: In this paper we describe the Nimrod/O design optimization tool, and its application in computational fluid dynamics. Nimrod/O facilitates the use of an arbitrary computational model to drive an automatic optimization process. This means that the user can parameterise an arbitrary problem, and then ask the tool to compute the parameter values that minimize or maximise a design objective function. The paper describes the Nimrod/O system, and then discusses a case study in the evaluation of an aerofoil problem. … Show more

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Cited by 46 publications
(34 citation statements)
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“…The figure shows the performance of square matrix multiplication (of size 800 × 800) as a function of tiling and unrolling factors. The search space is not smooth and contains multiple 1 Tiling loop transformation partitions a loop nest's iteration space into small blocks and then iterates through those blocks in sequence. The goal is to maintain a small data footprint for the sub-loop nests for better cache usage.…”
Section: Motivationmentioning
confidence: 99%
See 3 more Smart Citations
“…The figure shows the performance of square matrix multiplication (of size 800 × 800) as a function of tiling and unrolling factors. The search space is not smooth and contains multiple 1 Tiling loop transformation partitions a loop nest's iteration space into small blocks and then iterates through those blocks in sequence. The goal is to maintain a small data footprint for the sub-loop nests for better cache usage.…”
Section: Motivationmentioning
confidence: 99%
“…The Nelder-Mead Simplex algorithm [61], is one of the most widely used direct search methods in auto-tuning systems [1,23,35]. We provide a high-level description of the algorithm in chapter 3.…”
Section: Search Algorithmsmentioning
confidence: 99%
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“…Flow around an airfoil was modelled, [8], using the computational fluid dynamics package FLUENT. Input parameters were the thickness, camber and angle of attack of the airfoil; the aim was to maximize the ratio of lift to drag.…”
Section: Airfoilmentioning
confidence: 99%