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31. The authors of this paper developed a transient temperature measurement system of burnt gas in a combustion chamber based on the theory of absorption-emission.

32. This inhibiting of flow oscillations adds stability to the combustion chamber.

33. As the air inlet diameters increase, the intake central swirl is intensified and thus fuel evaporation in the first combustion chamber is improved.

34. The authors consider that increasing the piston stroke is an effective scheme, and point out that the petaloid combustion chamber has a good adaptability.

35. The results shoW that the carbon deposit layer on the combustion chamber has strong isolative effect on the transient heat transfer between working medium and the parts of combustion chamber.

36. The geometry of the combustion chamber and the atomisation of the fuel a decisive role here.

37. In the paper, matching tests were made for different combustion chamber geometries, injection pressure levels and injection nozzle configurations in a 6110 type diesel engine.

38. Air at atmospheric pressure is sucked into the combustion chamber.

39. It can provide a powerful tool for the engineering analysis ofgeometry optimization for the combustion chamber.

40. The semi-vertical reverberatory furnace comprises a combustion chamber, a forehearth part, a vertical furnace and an aeration tower.

41. It can calculate effectively the variation of flame front area, burned volume, and heat transfer area with the process of flame propagation and can be applied to an arbitrary combustion chamber.

42. Increasing the intensity of intake swirl could improve the evaporation rate of the fuel on the wall of the combustion chamber, but the NOX emission increases.

43. Calculates the example for the two-dimensional combustion chamber compressible flow field.

44. The results of the calculation and the analysis of effects of combustion chamber pressure, mixture ratio, propellant injection temperature and injector type on the combustion processes are reported.

45. A perfectly stirred reactor model was adopted for its combustion chamber; and the steady quasi-1D isentropic flow was used for the nozzle flow.

46. The clogging of a briquet hole is prevented; a plurality of combustible gas is provided for the combustion chamber, promoting the sufficient combustion of the briquet.

47. All of which will offer automatism control of gas flux, flux of spelter liquid and temperature of venting fumes in combustion chamber assort of referenced basis .

48. For the simplified system was applied in a constant volume combustion chamber, the combustible mixture can be ignited at any situation.

49. The spark plug is installed in the combustion chamber of the gasoline engine and used to ignite the compressed combustible mixture in the cylinder.

50. It puts forward an effective deep drawing technology about the alloy board with low-alloy and high-strength so that the properties of motor combustion chamber case satisfy with the needs of system.

51. Combustion instability not only affects the stability of the aero-engine work, but also caused the combustion chamber flame tube thin-walled structure acoustic-vibration coupled fatigue.

52. The axial distribution of fuel vapor near combustion chamber wall surface can be improved by changing nozzle spray angle to improve engine combustion.

53. The cold smoke is the result of access of excessive engine oil into the combustion chamber, but fail to burning after evaporation.

54. Given sufficient turbulence in the combustion chamber,[http://Sentencedict.com] detonation is unlikely to occur.

55. The strong squish flow and vortexes produced by the special structure of the combustion chamber improve the fuel and air mixture and combustion spe...

56. The results are important to design combustion chamber geometry and control combustion stability.

57. It's beneficial to improve combustion rate of pulverized coal that Alance was fixed while Blance was moved away combustion chamber from reference location.

58. This paper presents a finite-volume method for flow characteristics simulation in a combustion chamber with a flat-topped piston during the compression stroke.

59. A new modular method for calculating the maximum combustion chamber pressure with stage combustion cycles is proposed in this paper.

60. Note that the compression ratios shown above reflect the expansion ratio, which is the ratio of the combustion chamber volumes when the piston is at Bottom dead centre and Top dead centre.