Fluidics Jet Vectoring for Incompressible Flow by Using Counter Flow Method for Circular Duct

Authors

  • Ali A-M. H. AlAsadi Dep. of Mechanical Engineering, College of Engineering, Baghdad University
  • Ahmed Hikmat Faseeh Dep. of Mechanical Engineering, College of Engineering, Baghdad University

Keywords:

Thrust Vectoring, Jet vectoring angle, Coanda effect, Counter-flow, mass flow ratio

Abstract

Computational and experimental investigation of fluidic thrust vectoring using counter-flow method had been carried out in the present work. The experimental investigation involved the design and construction of a test rig for a circular duct to examine the effect of various geometric variables on the thrust vectoring angle. The experimental tests covered Coanda surface radius R/d = (0.58823, 1.17647, 1.75471), secondary gap height h/d = (0.02941, 0.05882), over a secondary mass flow ratio range (0 ?

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Published

01-08-2017

Issue

Vol. 20 No. 4 (2017): Al-Nahrain Journal for Engineering Sciences

Section

Articles

License

The authors retain the copyright of their manuscript by submitting the work to this journal, and all open access articles are distributed under the terms of the Creative Commons Attribution-NonCommercial 4.0 International (CC-BY-NC 4.0), which permits use for any non-commercial purpose, distribution, and reproduction in any medium, provided that the original work is properly cited.

How to Cite

[1]
A. A.-M. H. AlAsadi and A. H. Faseeh, “Fluidics Jet Vectoring for Incompressible Flow by Using Counter Flow Method for Circular Duct”, NJES, vol. 20, no. 4, pp. 911–923, Aug. 2017, Accessed: Dec. 22, 2024. [Online]. Available: https://nahje.com/index.php/main/article/view/316

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