Comparison of alcogas aviation fuel with export aviation gasoline

Mixtures of gasoline and alcohol when used in internal combustion engines designed for gasoline have been found to possess the advantage of alcohol in withstanding high compression without "knock" while retaining advantages of gasoline with regard to starting characteristics. Test of such fuels for maximum power-producing ability and fuel economy at various rates of consumption are thus of practical importance, with especial reference to high-compression engine development. This report discusses the results of tests which compares the performance of alcogas with x gasoline (export grade) as a standard

Fractional Generalization of Gradient Systems

We consider a fractional generalization of gradient systems. We use differential forms and exterior derivatives of fractional orders. Examples of fractional gradient systems are considered. We describe the stationary states of these systems.Comment: 11 pages, LaTe

Financial Consequences of Ill Health and Informal Coping Mechanisms in Indonesia

We assess the financial risk of ill health for households in Indonesia, the role of informal coping strategies, and the effectiveness of these strategies in smoothing consumption. based on household panel data, we find evidence of financial risk from illness through medical expenses, while income from informal wage labor is exposed to risk for the poor and income from self-employed business activities for the non-poor. however, only for the rural population and the poor does this lead to imperfect consumption smoothing, while the non-poor seem to be able to protect current spending. borrowing and drawing on buffers, such as savings and assets, seem to be key informal coping strategies for the poor, which infers potential negative long term effects. while these results suggest scope for public intervention, the financial risk from income loss for the rural poor is beyond public health care financing reforms. rather, formal sector employment seems to be a key instrument for financial protection from illness, by also reducing income risk. key words: illness, income, consumption smoothing, coping strategies, Indonesia jel: o15, i1

On the recurrence and robust properties of Lorenz'63 model

Lie-Poisson structure of the Lorenz'63 system gives a physical insight on its dynamical and statistical behavior considering the evolution of the associated Casimir functions. We study the invariant density and other recurrence features of a Markov expanding Lorenz-like map of the interval arising in the analysis of the predictability of the extreme values reached by particular physical observables evolving in time under the Lorenz'63 dynamics with the classical set of parameters. Moreover, we prove the statistical stability of such an invariant measure. This will allow us to further characterize the SRB measure of the system.Comment: 44 pages, 7 figures, revised version accepted for pubblicatio

Entropy production in boundary layers

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77333/1/AIAA-197-774.pd

Incompressible Turbulent Flow in a Permeable-Walled Duct

An analysis is made of fully developed turbulent flow in a paralle

Thermodynamic formalism for contracting Lorenz flows

We study the expansion properties of the contracting Lorenz flow introduced by Rovella via thermodynamic formalism. Specifically, we prove the existence of an equilibrium state for the natural potential $\hat\phi_t(x,y, z):=-t\log J_{(x, y, z)}^{cu}$ for the contracting Lorenz flow and for $t$ in an interval containing $[0,1]$. We also analyse the Lyapunov spectrum of the flow in terms of the pressure

Radiating Effectiveness of Annular-Finned Space Radiators, Including Mutual Irradiation between Radiator Elements

the authors also provide an approximate quantitative number for the accuracy of the numerical results. Based on the authors' results of Figs. 8 and 9, the fully developed periodic flow is achieved at x/L = 4 and 30 for Re = 200 and 1600 respectively for L/H = 1. Would the authors first quantitatively define the periodic fully developed flow, and then provide the tabular values of x/L as functions of L/H and Re for L/H = 0.2,0.5,1,2 and 5, and the covered range of Re. A research task remains further refining the analytical model to correlate better the performance of interrupted wall surface with the experimental results. Subsequently, the more complex heat exchanger surfaces could be analyzed. In the meanwhile, this paper by Prof. Sparrow and his colleagues serves as a reminder that the flow and heat transfer phenomena in a compact heat exchanger are too complex to analyze. A better quantitative understanding of the flow phenomena is essential for better correlations and improved heat exchanger design. Additional Reference Authors' Closure We are appreciative of the perspectives conveyed by Dr. Shah's Discussion. With regard to the role of vortices and wakes, there are, assuredly, conditions where they will affect both the heat transfer and friction. On the other hand, there are conditions for which no significant effect will be felt. Perspectives on these conditions are conveyed in references [11] and [12]. In connection with the identification of the periodically developed regime in Figs. 8 and 9, there is considerable latitude depending on the selected criterion. Since all portions of a velocity or temperature profile do not develop with equal rapidity, there are various criteria that can be employed. It was for this reason that we did not quote development lengths in the paper. Additional References 11 Kottke, V., Blenke, H., and Schmidt, K. G., "The Influence of Nose Section and Turbulence Intensity on the Flow Around Thick Plates in Parallel Flow," Warme-und Stoffubertragung, Vol. 10,1977, pp. 159-174. 12 Loehrke, R. I., Roadman, R. E., and Read, G. W" ASME Paper The purpose of this discussion is to point out how one of Minning's results can be generalized. In his analysis of the inverted conical frustrum, Minning has chosen to express his results in terms of four variables-the cone half angle fi, the height of the frustrum h, the radial location of the differential element p, and the vertical distance from the differential element to the extended frustrums' vertex s. In my view, this last choice is not the natural one and indeed it obscures the generality of the result expressed by equation It appears that a better choice of variable would be the radius of the frustrum in the plane of the element or ring, which is given by r = -s tan fi. If s is thereby eliminated from equation With respect to this latter point, one may note, as was done for a cylinder by Sparrow, et al. [1] that the shape factor in question can be considered as the sum of two parts-one being a circular segment and, in this case, the other being a tilted triangular plate frustrum. 1 By C. P. Minning, published in the August, 1977 issue of the JOURNAL OP HEAT TRANSFER, Vol. 99, No. 3, The Aerospace Corporation, El Segundo, CA 90245. Since the former is known [2], the latter can be readily obtained and subsequently expressed in variables more suitable for that configuration. This, of course, introduces new possibilities too numerous to mention. Finally, since Minning does not mention any analytical checks of his result, it is pointed out that, when /3 = 0, it reduces to a form equivalent to that for the cylinder [1]. Additional References 1 Sparrow, E. M., Miller, G. B., and Jonsson, V. K., "Radiating Effectiveness of Annular-Finned Space Radiators, Including Mutual Irradiation between Radiator Elements," Journal Aerospace Sciences, Vol. 29, 1962, pp. 1291-1299 2 Sparrow, E. M., "A New and Simpler Formulation for Radiative Angle Factors," ASME JOURNAL OF HEAT TRANSFER, Vol. 85,1963, pp. 81-88. Author's Closure I appreciate Dr. Nelson's pointing out that the applicability of equation An alternate expression that avoids this confusion can be derived by substitution of the relation r = -s tanjtf, as suggested by Dr. Nelson, and the relation a = (7r/2) -fi into equation C^)] [(h cot a + r) -In this expression, a is the angle between the plane of dAi and the sloping side of the conical frustrum. Values of a are always positive and lie in the range 0 < « < TT. For 0 < « < 7r/2, the frustrum opens upward away from the plane of dA\. For 7r/2 < a < w, the frustrum opens downward toward the plane of dAi. The special case, a = it 12