By R. W. Bilger (auth.), Prof. Richard S. L. Lee, Prof. James H. Whitelaw, Prof. T. S. Wung (eds.)
A Symposium on Aerothermodynamics of Combustors used to be held on the Institute of utilized Mechanics of the nationwide Taiwan collage from three to five June 1991 and used to be attended through one hundred thirty delegates from 8 nations. the themes of the 40 formal displays integrated measurements and calculations of isothermal simulations and of combusting flows with one and stages, and with attention of configurations starting from easy diffusion to gas-turbine flows. The discussions in and out of the Symposium corridor have been vigorous and an open discussion board consultation proven the variety of evaluations presently and strongly held. The overseas Union of Theoretical and utilized Mechanics initiated the Symposium lower than the chairmanship of Professor R S L Lee and with the clinical Committee indexed under. It benefited from sponsorship, back as indexed lower than, and from members who awarded fascinating and updated descriptions in their learn. Invited lectures have been introduced via Professors R Bilger and F Weinberg and set the scene when it comes to caliber of fabric and presentation.
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Additional resources for Aerothermodynamics in Combustors: IUTAM Symposium Taipei, Taiwan, 1991
The tomographic method with a thin laser sheet reveals the instantaneous shape of the cross section of the unburned mixture region. Figure 12 shows three examples of the image processed tomographic pictures taken at different instances. The experimental conditions are almost same as those of Fig. ll(b). As in the schlieren photographs. the boundaries between the unburned mixture jets and the recirculation zones are recognizable. It is seen that a tongue of the unburned mixture spreads into the burned gas region.
In the estimation of the turbulence Reynolds numbers and the Damkohler numbers, there is one problem, because the turbulence characteristics 34 vary significantly in space. We used in the estimation the values of u', L and A at the center plane and just in front of the turbulent flame zone . Therefore, all of the information pertain to order of magnitude estimates, not to uniquely defined, precise quantities. A typical value of R A ranges from 300 to 1300 and that of Da from 5 to 25. Gas Loser computer VTR -i Water Supply I ceo Camero Propane Suppl y Air Suppl y Burner Ti(OH)4 Supp l y FigA.
0 -0. 70 ~ -16. ________________________--____________ -12. -8. o. -4. ~-- 4. __________--________ 8. ~ 12. 16. z(mm) Fig. 14: Axial profiles of the tl (radial) component of the velocity field at different r locations Fig. 14 shows the u-distribution as a function of z for various r locations. Around Zo and for - 12 mOl < r < 12 mOl, a constant 311/3z = 0 region is observed. The above described general features of the flow remain valid for all the flow cases. The Zo position of the stagnation plane is different in each of the cases as seen from Table 1.