Impact of the nozzle angle, distance between burners, and N2 on burning velocity of the diffusoin counter flames

Joint Authors

Umar, Salwa Tariq
Abd al-Karim, Jasim Muhammad
Salih, Fuad Ulwan

Source

Journal of Engineering and Sustainable Development

Issue

Vol. 24, Issue 3 (31 May. 2020), pp.29-42, 14 p.

Publisher

al-Mustansyriah University College of Engineering

Publication Date

2020-05-31

Country of Publication

Iraq

No. of Pages

14

Main Subjects

Mechanical Engineering

Topics

Abstract EN

The achievement of precise measurements on the laminar diffusion flames plays a big role in the process of realizing a wide flames range.

Despite most of fuel is likely burnt in the turbulent combustion, there is still data requirement for the data on the velocities of the laminar burning as input to several models of the turbulent combustion.

And, in engines with an internal combustion, the first combustion is laminar, thus once more, there is a requirement for the velocity of the laminar burning.

The burning velocity of the laminar diffusion flame was measured at three nozzles at different angles (30º, 45º, and 60º) and different distances between the nozzles burners (H = 20, 30, and 40 mm) with and without the N2, and wide range of equivalence ratios (0.65 ≤ϕ≤ 1.5).

Schlieren photographs were captured to qualitatively assess the effect of angle of nozzles, distance, and N2 on the burning velocity of the diffusion flame.

Burning velocity depends on the stagnation surface of the flame front, which in turn relies on the vertical distance (H) between the burners.

Also, it was noticed that the increase in distance between the burners leads to a decrease in the velocity of the reactants since it is affected by the air The achievement of precise measurements on the laminar diffusion flames plays a big role in the process of realizing a wide flames range.

Despite most of fuel is likely burnt in the turbulent combustion, there is still data requirement for the data on the velocities of the laminar burning as input to several models of the turbulent combustion.

And, in engines with an internal combustion, the first combustion is laminar, thus once more, there is a requirement for the velocity of the laminar burning.

The burning velocity of the laminar diffusion flame was measured at three nozzles at different angles (30º, 45º, and 60º) and different distances between the nozzles burners (H = 20, 30, and 40 mm) with and without the N2, and wide range of equivalence ratios (0.65 ≤ϕ≤ 1.5).

Schlieren photographs were captured to qualitatively assess the effect of angle of nozzles, distance, and N2 on the burning velocity of the diffusion flame.

Burning velocity depends on the stagnation surface of the flame front, which in turn relies on the vertical distance (H) between the burners.

Also, it was noticed that the increase in distance between the burners leads to a decrease in the velocity of the reactants since it is affected by the air surrounding.

American Psychological Association (APA)

Umar, Salwa Tariq& Salih, Fuad Ulwan& Abd al-Karim, Jasim Muhammad. 2020. Impact of the nozzle angle, distance between burners, and N2 on burning velocity of the diffusoin counter flames. Journal of Engineering and Sustainable Development،Vol. 24, no. 3, pp.29-42.
https://search.emarefa.net/detail/BIM-1263675

Modern Language Association (MLA)

Umar, Salwa Tariq…[et al.]. Impact of the nozzle angle, distance between burners, and N2 on burning velocity of the diffusoin counter flames. Journal of Engineering and Sustainable Development Vol. 24, no. 3 (May. 2020), pp.29-42.
https://search.emarefa.net/detail/BIM-1263675

American Medical Association (AMA)

Umar, Salwa Tariq& Salih, Fuad Ulwan& Abd al-Karim, Jasim Muhammad. Impact of the nozzle angle, distance between burners, and N2 on burning velocity of the diffusoin counter flames. Journal of Engineering and Sustainable Development. 2020. Vol. 24, no. 3, pp.29-42.
https://search.emarefa.net/detail/BIM-1263675

Data Type

Journal Articles

Language

English

Notes

-

Record ID

BIM-1263675