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Elangovan, S.
- Computational Analysis of Mixing Characteristics of Jets from Rectangular Nozzle with Internal Grooves
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Authors
Affiliations
1 Department of Aeronautical Engineering, Bharath University, Chennai-600 073, IN
1 Department of Aeronautical Engineering, Bharath University, Chennai-600 073, IN
Source
Indian Journal of Science and Technology, Vol 6, No S5 (2013), Pagination: 4543-4548Abstract
A Computational study has been carried out to understand jet flow development from plain and grooved rectangular nozzles of aspect ratio 2:1. Grooves of square cross section of side 4mm and axial length 5mm were introduced at the exit of the nozzle in three different orientations as (i) minor-axis, (ii) major-axis and, (iii) in both minor and major axes. The computational studies were carried out using computational software ANSYS CFX for a nominal jet exit velocity of 20m/s. Velocity distribution along the axis of the jet is observed from computational results and compared with the available experimental results. Grooves seem to have very negligible effect on the near field region but significantly influence the jet decay in the far field.Keywords
Passive Control, Jet Mixing Enhancement, Rectangular Jet and Center Line Velocity DecayReferences
- Ho C M, and Gutmark E J (1987). Vortex induction and mass entrainment in a small-aspect ratio elliptic jet, Journal of Fluid Mechanics, vol 179, 383–405.
- Hussain H S, and Husain A K M F (1989). Elliptic jets part I: characteristics of unexcited and excited jets, Journal of Fluid Mechanics, vol 208, 257–319.
- Verma S B, and Rathakrishnan E (1998). Mixing enhancement and noise attenuation in notched elliptic-slot jets, International Journal of Turbo and Jet Engines, vol 15, 7–25.
- Srinivasan K, and Rathakrishnan E (1985). Studies on polygonal slot jets, AIAA Journal, vol 38, No. 10.
- Elangovan S, and Rathakrishnan E (2004). Studies on high speed jets from nozzles with internal grooves, The Aeronautical Journal, vol 108, 43–50.
- Arunkumar P, Verma S B et al. (2011). Study of jets from rectangular nozzles with square grooves, The Aeronautical Journal, vol 115, 187–196.
- Pao S P, and Abdol K S (1996). Numerical simulation of jet aerodynamics using the three-dimensional Navier-stokes code PAB3D, NASA Technical Paper, NASA TP-3596, 1–43.
- Similarity Analysis of Pressure Distribution along the Wake Axis of Elliptic Cones
Abstract Views :226 |
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Authors
Affiliations
1 Department of Aeronautical Engineering, Bharath University, Agaram Then Road, Selaiyur, Chennai, IN
2 Department of Aerospace Engineering, Madras Institute of Technology Campus, Anna University, Chromepet, Chennai, IN
1 Department of Aeronautical Engineering, Bharath University, Agaram Then Road, Selaiyur, Chennai, IN
2 Department of Aerospace Engineering, Madras Institute of Technology Campus, Anna University, Chromepet, Chennai, IN
Source
Indian Journal of Science and Technology, Vol 7, No S5 (2014), Pagination: 56-60Abstract
The Effect of freestream velocity and Ellipticity ratio on the similarity distribution of the static pressure along the wake axis of the elliptic cones is presented. A cone of elliptic cross section produces separated flow at the downstream of its base. Within the separated region the flow is observed to be opposite (reverse) to the main outer flow. To obtain the length of reverse flow region, magnitude and location of maximum reverse velocity and re attachment point knowledge of pressure distribution behind a body is essential. Experiments were carried out for three different test section freestream velocities 6m/s, 15m/s and 25 m/s (Reynolds numbers 0.16 x 105, 0.4 x 105 and 0.667 x 105 based on cone effective diameter respectively). Ellipticity ratio 1 and 3 with constant fineness and bluntness ratio of 2.75 and 0.049 respectively were considered for the experiments. A Digital Sensor Array -DSA was used for static pressure measurements. The pressure sensor has the capability of 1 PSI differential pressure range with +/- 0.12% full-scale accuracy. Good similarity in wake axis static pressure distribution is noted for different freestream velocity behind a circular cone. But, Similarity in pressure distribution is not observed along the wake axis of an elliptic cone at tested lower freestream velocity (6 m/s).Keywords
Elliptic Cone, Pressure Coefficient And Similarity Parameter, Wake Pressure- Effect of Rib Geometry on the Base Pressure of Suddenly Expanded Flows
Abstract Views :210 |
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Authors
Affiliations
1 Department of Aeronautical Engineering, Bharath University, Agaram then road, Selaiyur, Chennai, Tamil Nadu, IN
1 Department of Aeronautical Engineering, Bharath University, Agaram then road, Selaiyur, Chennai, Tamil Nadu, IN
Source
Indian Journal of Science and Technology, Vol 7, No S5 (2014), Pagination: 61-63Abstract
Suddenly expanded flows find application in various engineering devices. The flow in the sudden expansion region is found to be affected by various factors. Passive control methods like protruding ribs are found to be very effective in the control of suddenly expanding flows. In the present study the effect of geometry of ribs on the flow characteristics is investigated computationally. The rib geometries studied are rectangular of two aspect ratios, circular, semicircular and triangular. The computational results show that rectangular rib of aspect ratio 3 significantly reduced the base pressure. The results compare very well with experimental results.- Assessment of Air Quality Index of Coimbatore City in Tamil Nadu
Abstract Views :170 |
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Authors
Affiliations
1 Department of Mechanical Engineering, KPR Institute of Engineering and Technology, Coimbatore - 641407, Tamil Nadu, IN
2 Environmental Division, Public Works Department, Coimbatore Division, Coimbatore, Tamil Nadu, IN
1 Department of Mechanical Engineering, KPR Institute of Engineering and Technology, Coimbatore - 641407, Tamil Nadu, IN
2 Environmental Division, Public Works Department, Coimbatore Division, Coimbatore, Tamil Nadu, IN