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

Authors(3) :-Dr P V Senthiil, VS Mirudhuneka, Aakash

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.

Authors and Affiliations

Dr P V Senthiil
Head, Advance Manufacturing Technology ,Mechanical Engineering, St.Peters University,Chennai, Tamilnadu, India
VS Mirudhuneka
SAP Consultant, IBM Ltd, Porur, Chennai, Tamilnadu, India
Aakash
Department of Mech, SRM University, Chennai, Tamilnadu, India

Jet nozzle, performance analysis, iinletparameters,optimization

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


Publication Details

Published in : Volume 1 | Issue 1 | January-Febuary 2015
Date of Publication : 2015-02-25
License:  This work is licensed under a Creative Commons Attribution 4.0 International License.
Page(s) : 237-242
Manuscript Number : IJSRSET151150
Publisher : Technoscience Academy

Print ISSN : 2395-1990, Online ISSN : 2394-4099

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.
Journal URL : http://ijsrset.com/IJSRSET151150

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