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Design and Performance Analysis of Single Inlet Multiple Outlet Jet Nozzle with Thrust Vector Control

Authors(3):

Dr P V Senthiil, VS Mirudhuneka, Aakash
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Today, thrust vectoring has become a very important research subject which can dramatically change the way aircraft maneuver and its performance. This paper tries to present a unique approach to this topic by highlighting a concept defined as Single Inlet Multiple Outlet (SIMO) in detail. This can be explained by having multiple nozzles for exhaust purpose than those conventional one or two nozzles as we know of presently. This idea may yet not be able to apply directly to VTOL (Vertical Takeoff & Landing), but can be applied very well to change thrust direction of the aircraft effectively including thrust reversal and hence reducing the dependability on the primary control surface to great extent. These nozzles can be made to work in tandem with primary control surfaces so that, in case of failure of primary control surfaces occur, the aircraft can still be maneuvered and saved thereby avoiding loss of millions of dollar worth of property, aircraft and most important pilot’s life.

Dr P V Senthiil, VS Mirudhuneka, Aakash

Jet nozzle, performance analysis, iinletparameters,optimization

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1. Mr. Periyasamy, HOD, Production Engg, St.Peter’s University. 

2. Mr.Sengolerayan, HOD, Mechanical Engg, St.Peter’s University.

3. Dr. Chinnapandiyan, HOD, Aeronautical Engg, St.Peter’s University.

4. Mr.Jebamani, Asst.Professor,Mechanical Engg, St.Peter’s University.

5. Mr.D.David, Asst.Professor,Mechanical Engg, St.Peter’s University.

VI. REFERENCES

[1]. Thrust Vectoring Nozzlefor Modern Military Aircraftby DanielIkaza, Industria de Turbo Propulsores S.A. (ITP), Spain. 

[2]. STOL Aircraft Design for Undergraduates, Russell M Cummings, David W Hall.

[3]. Nozzle of air breathing engines, V.B.Rutovskii – Mascow state aviation institute, Russia.  

[4]. Highlights of the JSF X-35 STOVL Jet Effects Test Effort, Mark D Buchholz; Lockheed Martin Aeronautics Company, California, USA.

[5]. The F-22 Performance by Lockheed Martin Aeronautics Company.

[6]. International Council for Aeronautical Science – 441-2012

[7]. Jet engines by Rolls Royce. 

[8]. Wikipedia, the free online encyclopedia

[9]. www.grc.nasa.gov

[10]. www.airforce-technology.com (website for defense industries- Air force)

[11]. www.aerospaceweb.org 

[12]. www.answers.com


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Publication Details

Published in : Volume 1 | Issue 1 | January-Febuary - 2015
Date of Publication Print ISSN Online ISSN
2015-02-25 2395-1990 2394-4099
Page(s) Manuscript Number   Publisher
237-242 IJSRSET151150   Technoscience Academy

Cite This Article

Dr P V Senthiil, VS Mirudhuneka, Aakash, "Design and Performance Analysis of Single Inlet Multiple Outlet Jet Nozzle with Thrust Vector Control", International Journal of Scientific Research in Science, Engineering and Technology(IJSRSET), Print ISSN : 2395-1990, Online ISSN : 2394-4099, Volume 1, Issue 1, pp.237-242, January-Febuary-2015.
URL : http://ijsrset.com/IJSRSET151150.php