Affiliation:
1. Institute of Heat Engineering, Faculty of Power and Aeronautical Engineering , Warsaw University of Technology , Nowowiejska 21/25, 00-665 Warsaw
Abstract
Abstract
In this paper, the experimental results of a detonation chamber fed by air from a centrifugal compressor are presented. The detonation chamber was equipped with many different sensors, mostly thermocouples, which were placed in 11 different positions. The distribution of temperature changes along the chamber and radial temperature profile at the outlet are provided. The results here confirm the existence of high mixture stratification. Such mixture stratifications and temperature profiles may be used as an additional chamber wall cooling method. The experiments performed, address key issues regarding the chamber choking problem caused by turbines. The relationship between the turbine performance and detonation chamber are crucial for proper control of turbine jet engine.
Reference17 articles.
1. [1] Chapman D. L., 1899, “VI. On the rate of explosion in gases”, Philosophical Magazine Series 5, Volume 47, Issue 284, pp.90-104.10.1080/14786449908621243
2. [2] Jouguet E., 1905, “Sur la propagation des réactions chimiques dans les gaz” [On the propagation of chemical reactions in gases], Journal de Mathématiques Pures et Appliquées, series 6 (in French) 1: pp. 347–425.
3. [3] Nicholls J.A., Wilkinson, H.R., and Morrison, R.B., 1957, “Intermittent Detonation as a Thrust Producing Mechanism.”, Jet Propulsion, Vol. 27, pp. 534-541.10.2514/8.12851
4. [4] Kindracki J., 2008, „Badania eksperymentalne i symulacje numeryczne procesu wirującej detonacji gazowej” [Experimental research and numerical calculation of the rotating detonation], Ph.D. Thesis, Warsaw University of Technology (in polish)
5. [5] Kailasanath K., 2000, “Review of Propulsion Applications of Detonation Waves”, AIAA Journal, Vol. 38, No. 9, pp. 1698-1708, http://dx.doi.org/10.2514/2.1156.10.2514/2.1156
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