The S-Shaped Utility Function
In: Synthese: an international journal for epistemology, methodology and philosophy of science, Band 135, Heft 2, S. 243-272
ISSN: 1573-0964
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In: Synthese: an international journal for epistemology, methodology and philosophy of science, Band 135, Heft 2, S. 243-272
ISSN: 1573-0964
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In: SIAM J. Control Optim., 58(6), 3734-3762.
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In: American Journal of Agricultural Economics, Band 82, Heft 1, S. 49-58
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In: Water Utility Management Journal, Band Vol.1(1), S. 8-11
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In: Acta polytechnica: journal of advanced engineering, Band 41, Heft 4-5
ISSN: 1805-2363
This paper examines the flow in a diffusing s-shaped aircraft air intake using computational fluid dynamics (CFD) simulations. Diffusing s-shaped ducts such as the RAE intake model 2129 (M2129) give rise to complex flow patterns that develop as a result of the offset between the intake cowl plane and engine face plane. Euler results compare favourably with experiment and previous calculations for a low mass flow case. For a high mass flow case a converged steady solution was not found and the problem was then simulated using an unsteady flow solver. A choked flow at the intake throat and complex shock reflection system, together with a highly unsteady flow downstream of the first bend, yielded results that did not compare well with previous experimental data. Previous work had also experienced this problem and a modification to the geometry to account for flow separation was required to obtain a steady flow.RANS results utilising a selection of turbulence models were more satisfactory. The low mass flow case showed good comparison with experiment and previous calculations. A problem of the low mass flow case is the prediction of secondary flow. It was found that the SST turbulence model best predicted this feature. Fully converged high mass flow results were obtained. Once more, SST results proved to match experiment and previous computations the best. Problems with the prediction of the flow in the cowl region of the duct were experienced with the S-A and k-w models. One of the main problems of turbulence closures in intake flows is the transition of the freestream from laminar to turbulent over the intake cowl region. It is likely that the improvement in this prediction using the SST turbulence model will lead to more satisfactory results for both high and low mass flow rates.
In: History of political economy, Band 46, Heft 2, S. 231-246
ISSN: 1527-1919
The concept of utility, which stood at the heart of J. S. Mill's utilitarian moral philosophy, played only a minor role in his account of economics. The economic idea of (individual) utility, as is well known, neither inspired Mill directly nor excited his attention when developed in the work of other economists. The starting point of this article is thus the question of just why was Mill so interested in utility as a seminal concept of moral philosophy but seemingly indifferent to (individual) utility as an economic concept. I argue that Mill's determination to strengthen and enrich the concept of utility in his moral philosophy ironically largely precluded any development within his political economy of an idea of utility related to a psychological effect within the individual mind; in particular, this is due to the potential of such an interpretation to create an unwelcome obstacle in his struggle with the Romantic critics of utilitarianism.
In: Materials and design, Band 235, S. 112442
ISSN: 1873-4197