Open Access Open Access  Restricted Access Subscription Access
Open Access Open Access Open Access  Restricted Access Restricted Access Subscription Access

Flow Investigation through a Curved Square S-Duct


Affiliations
1 National Institute of Technology, Durgapur 713 209, West Bengal, India
2 Durgapur Institute of Advanced Technology & Management, West Bengal, India
     

   Subscribe/Renew Journal


This paper presents the results of an experimental work with measurement of wall static pressure of 45°/45° S shaped curved duct. An S shaped duct is widely used in aircraft intakes, gas turbines. The test ducts are made up of transparent perspex sheets to facilitate the flow visualization study. The duct have inlet to exit area ratio of 1.0 with centerline distance of 0.75m. The inlet aspect ratio of the test duct has been fixed at 1.0 with inlet width 100mm. The velocities for the proposed investigations are to be measured by using calibrated Pitot tube. Wall pressures are measured with the help of inclined manometer with the inclination of 35°. The main purpose of this investigation is to show the development of secondary flow which happens when flow takes place through the bend in the curvature. This secondary flow arises as a result of centrifugal force acting when the flow moves through the bend. The investigation is carried out at three different velocities 20 m/s, 40 m/s, 60 m/s. The distribution of normalized pressure which is the ratio of static pressure to the dynamic pressure is mapped and shown in the form of contours by using the software package SURFER. The trend of wall static pressure development on the walls of S shaped duct shows that as the flow proceeds towards the curvature and there exists a high pressure gradient between the outside face and inside face due the centrifugal force acting at the curvature. This shows the bulk shifting of flow towards outside face. This is due to the generation of secondary motion in a plane perpendicular to the primary flow. This gradient becomes zero at the inflexion plane. After the inflexion, the change of curvature causes a reverse trend in the wall static pressure growth leading to the probable development of pair of contra-rotating vortices as a result of secondary motion with opposite sense of rotation compared to the first half of the bend.

Keywords

45°/45° S Shaped Curved Duct, Secondary Flow, Contra-Rotating Vortices, SURFER.
User
Subscription Login to verify subscription
Notifications
Font Size

  • Bansod, P. and Bradshaw, P., The Flow in S shaped Ducts, Aeronautical Quarterly, Vol. 23, pp.131-140, 1972.
  • Brithford, K.M., Manners, A.P., McGuirk, J.J. and Stevens, S.J., Measurement and prediction of flow in annular S-shaped ducts, Experimental Thermal and Fluid Science, Vol. 9, No. 2, pp. 197-205, 1994.
  • Recheirt, B.A. and Wendt, B.J., An Experimental Investigation of S-Duct Flow Control Using Arrays of Low-Profile Vortex Generators, 31st Aerospace Sciences Meeting and Exhibit sponsored by the American Institute of Aeronautics and Astronautics Reno, Nevada, January 11-14, 1993.
  • Aslan and Samet, Experimental and Numerical Investigation of an S-duct diffuser that is designed for a Micro Turbojet Engine Powered Aircraft, January 2017.
  • Sonada, T., Arima T. and Oana. M., The Influence of Downstream Passage on the Flow within an Annular S-Shaped Duct, Trans ASME, Journal of Turbo Machinery, Vol.120, pp.714-722, 1998.
  • Taylor, A.M.K.P., Whitelaw J.H. and Yianneskis, M., Developing Flow in S-curved Ducts, Part 2-Circular Cross-Section Duct, NASA Contract Report No.3759. 1984,
  • Welborn, S.R., Reichert B.A., and Okishi, T.H., An Experimental Investigation of the Flow in a Diffusing S-Duct, NASA Technical Memorandum 105809, AIAA-92-3622, 28th Joint Propulsion Conference and Exhibit cosponsored by the AIAA, SAE, ASME and ASEE, Nashville, Tennessee, July 6-8, 1992.
  • Yu, S.C.M., Turbulent flow calculation in S-shaped diffusing ducts using viscous marching technique. 6th International Conference on Computational Method and Experimental Measurements, vol. 1: Heat and Fluid flow, edited by C.A. Brebbia and G.M. Carlamgro, Computational Mechanics Publications, Southampton Boston, co- published with Elsevier Allied Science, New York, 1993.

Abstract Views: 290

PDF Views: 17




  • Flow Investigation through a Curved Square S-Duct

Abstract Views: 290  |  PDF Views: 17

Authors

Niraj Kr. Prasad
National Institute of Technology, Durgapur 713 209, West Bengal, India
A. K. Biswas
National Institute of Technology, Durgapur 713 209, West Bengal, India
Prasanta K. Sinha
Durgapur Institute of Advanced Technology & Management, West Bengal, India

Abstract


This paper presents the results of an experimental work with measurement of wall static pressure of 45°/45° S shaped curved duct. An S shaped duct is widely used in aircraft intakes, gas turbines. The test ducts are made up of transparent perspex sheets to facilitate the flow visualization study. The duct have inlet to exit area ratio of 1.0 with centerline distance of 0.75m. The inlet aspect ratio of the test duct has been fixed at 1.0 with inlet width 100mm. The velocities for the proposed investigations are to be measured by using calibrated Pitot tube. Wall pressures are measured with the help of inclined manometer with the inclination of 35°. The main purpose of this investigation is to show the development of secondary flow which happens when flow takes place through the bend in the curvature. This secondary flow arises as a result of centrifugal force acting when the flow moves through the bend. The investigation is carried out at three different velocities 20 m/s, 40 m/s, 60 m/s. The distribution of normalized pressure which is the ratio of static pressure to the dynamic pressure is mapped and shown in the form of contours by using the software package SURFER. The trend of wall static pressure development on the walls of S shaped duct shows that as the flow proceeds towards the curvature and there exists a high pressure gradient between the outside face and inside face due the centrifugal force acting at the curvature. This shows the bulk shifting of flow towards outside face. This is due to the generation of secondary motion in a plane perpendicular to the primary flow. This gradient becomes zero at the inflexion plane. After the inflexion, the change of curvature causes a reverse trend in the wall static pressure growth leading to the probable development of pair of contra-rotating vortices as a result of secondary motion with opposite sense of rotation compared to the first half of the bend.

Keywords


45°/45° S Shaped Curved Duct, Secondary Flow, Contra-Rotating Vortices, SURFER.

References





DOI: https://doi.org/10.22485/jaei%2F2018%2Fv88%2Fi1-2%2F174922