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 was once attended by way of a hundred thirty delegates from 8 international locations. the subjects of the 40 formal displays integrated measurements and calculations of isothermal simulations and of combusting flows with one and levels, and with attention of configurations starting from easy diffusion to gas-turbine flows. The discussions inside and out of the Symposium corridor have been vigorous and an open discussion board consultation validated the variety of evaluations at the moment and strongly held. The overseas Union of Theoretical and utilized Mechanics initiated the Symposium below the chairmanship of Professor R S L Lee and with the medical Committee indexed lower than. It benefited from sponsorship, back as indexed under, and from individuals who provided attention-grabbing and updated descriptions in their examine. Invited lectures have been added by means of Professors R Bilger and F Weinberg and set the scene by way of caliber of fabric and presentation.
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Extra info for Aerothermodynamics in Combustors: IUTAM Symposium Taipei, Taiwan, 1991
9 symbols (*)). One can note (symbols (0)) that the nitrogen ring does not modify the central velocity profile. Fig. 10 shows a vector representation of the entire flow field obtained for H = 25 mm. It is found that two different asymmetric stable flows exist even if the same equal momentum condition are set up for each of the opposite outlet flows. A detailed analysis of the flow field show that, if the stagnation plane of one flow is located at zo' the other one is located at ·zo' Hence it is sufficient to discuss only one flow configuration.
25. : This Symposium. 26. : Princeton University, Private Communication (1991). 27. Tien, T. , This Symposium. 28. Gas Research Institute Digest,. 12 (1989) 22,38 29. : Combust. Sci. , 72 (1990) 101. 30. , Proc Roy Soc A418 (1988) 313. 31. : Combustion and Flame 78, (1989) 121. 32. ; Bradley, D. A. - 89 -2944 (1989). : Combustion Science and Technology, 70 (1990) 171. 34. : 23rd JANAF Combustion Meeting (October 1986). 35. ; 25th Joint propulsion Conference, paper no AIAA 89 -2564 (1989) 36. : 26th Joint Propulsion Conference, AIAA paper No.
The Doppler signal frequency was of the order of 200 kHz and the frequency shift applied through the Bragg cells was 200 kHz. These settings were found to be sufficient to avoid any loss of information by the filter settings but to assure a high percentage of signal acceptance. About 200 to 1000 validated signals per second were obtained at each measuring point depending on the instruments settings and on the location in the flow. To evaluate the final velocity, the digital signals from the counter were recorded hy a PDP 11/23 through a 16 bits Input/Output interface triffered by the data ready signal of the counter.