PL EN


Preferencje help
Widoczny [Schowaj] Abstrakt
Liczba wyników
Tytuł artykułu

Experimental studies of kerosene injection into a model of a detonation chamber

Autorzy
Wybrane pełne teksty z tego czasopisma
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
The paper presents results of experimental research of kerosene injection into high speed airflow of a model of a detonation chamber. Kerosene was injected into the rectangular section of the model’s chamber, which had a width of 20mm. A plain orifice kerosene injector of different diameters was used. The injector was set perpendicular to the airflow. The air was injected through a slot of a certain size that created the critical flow. Measurements of the air velocity distribution and numerical calculations for the chamber were performed in order to obtain data on the air speed inside the chamber. Measurements of the diameter of droplets injected into the model chamber were also taken. High-speed photography with a back light were utilized in the droplet diameter measurements. This provided information about the size of droplets and their spatial distribution
Rocznik
Strony
80--89
Opis fizyczny
Bibliogr. 7 poz., rys., wykr.
Twórcy
autor
  • Institute of Heat Engineering, Warsaw University of Technology, 21 / 25 Nowowiejska Street, 00-665 Warsaw, Poland
Bibliografia
  • [1] Tudosi A.: Aircraft gas-turbine engine’s control based on the fuel injection control, Chapter 11. In: Mulder M. (ed.): Aeronautics and Astronautics, 2011, InTech, pp. 305–330.
  • [2] Hamid A.H.A., Atan R.: Spray characteristics of jet–swirl nozzles for thrust chamber injector. Aerospace Science and Technology, 13, 2009, pp. 192–196.
  • [3] Liu Z., Reitz R.D.: An analysis of the distortion and breakup mechanisms of high speed liquid drops. International Journal of Multiphase Flow, 23(4), 1997, pp. 631–650.
  • [4] Wigley G., Heath J., Pitcher G., Whybrew A.: Experimental analysis of the response of a laser/phase doppler anemometer system to a partially atomized spray. Particle & Particle Systems Characterization, 18, 2001, pp. 169–178.
  • [5] Doungthip T., Ervin J.S., Williams T.F., Bento J.: Studies of injection of jet fuel at supercritical conditions. Industrial & Engineering Chemistry Research, 41, 2002, pp. 5856–5866.
  • [6] Al-Omari S.A.B.: Numerical simulation of liquid fuel sprays evolution and the subsequent vapor/air-mixture formation in a duct with a 90°-bend. International Communications in Heat and Mass Transfer, 35(2), 2008, pp. 197–203.
  • [7] Zakrzewski S., Milton B.E., Pianthong K., Behnia M.: Supersonic liquid fuel jets injected into quiescent air. International Journal of Heat and Fluid Flow, 25(5), 2004, pp. 833-840.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-5dac357f-bf6b-416b-ae46-e10fa496d882
JavaScript jest wyłączony w Twojej przeglądarce internetowej. Włącz go, a następnie odśwież stronę, aby móc w pełni z niej korzystać.