ISSN 2394-5125
 

Research Article 


THERMAL ANALYSIS AND DESIGN APPORACH OF JET ENGINE UNDER DIFFERENT ANALYTICAL PARAMETRIC CONDITIONS

I Venu Gopal.

Abstract
It is quite common that every component so designed will be affecting from various deformations and irregularities
which may lead to generation of various stresses. So, it is very much essential to analyze the component for various
stresses that are to be developed. Here, the analysis of various stresses in a turbojet engine is being done. The main
objective is to find out the Displacement, Equivalent and Fatigue stresses of the jet engine blades when subjected to
structural and thermal Loads. Structural analysis of a jet engine can be analyzed using finite element analysis
techniques In this work, a centrifugal type impeller has been designed using Ansys software to develop a pressure of
2.9 bar at the mass flow rate of 0.6 kg/s and suitable diffuser has been designed to guide the air flow in required
direction using the same software. According to the pressure and mass flow rate available annular type of
combustion chamber has been designed to produce suitable temperature. The turbine rotor, having reaction 0.4974
has been designed to produce the power required to run the impeller and the accessories in a single stage utilizing
the pressure and temperature available which has greatly reduced the cost of manufacturing. Aero foil shape
required for blade has been developed using Bludgeon tool of Ansys software. Impeller and diffuser have been
produced using Aluminum7078 by CNC machining. The flame holder provided inside the combustion chamber
stabilizes the flame thus initiating continuous combustion inside the combustion chamber. The flame holder used is
a baffle type flame holder because it is simple and efficient. The pulse jet body will be designed using the CATIA
V5 R20 software.

Key words: he pulse jet body will be designed using the CATIA V5 R20 software.


 
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Pubmed Style

I Venu Gopal. THERMAL ANALYSIS AND DESIGN APPORACH OF JET ENGINE UNDER DIFFERENT ANALYTICAL PARAMETRIC CONDITIONS. JCR. 2020; 7(17): 3353-3359. doi:10.31838/jcr.07.17.414


Web Style

I Venu Gopal. THERMAL ANALYSIS AND DESIGN APPORACH OF JET ENGINE UNDER DIFFERENT ANALYTICAL PARAMETRIC CONDITIONS. http://www.jcreview.com/?mno=16279 [Access: June 03, 2021]. doi:10.31838/jcr.07.17.414


AMA (American Medical Association) Style

I Venu Gopal. THERMAL ANALYSIS AND DESIGN APPORACH OF JET ENGINE UNDER DIFFERENT ANALYTICAL PARAMETRIC CONDITIONS. JCR. 2020; 7(17): 3353-3359. doi:10.31838/jcr.07.17.414



Vancouver/ICMJE Style

I Venu Gopal. THERMAL ANALYSIS AND DESIGN APPORACH OF JET ENGINE UNDER DIFFERENT ANALYTICAL PARAMETRIC CONDITIONS. JCR. (2020), [cited June 03, 2021]; 7(17): 3353-3359. doi:10.31838/jcr.07.17.414



Harvard Style

I Venu Gopal (2020) THERMAL ANALYSIS AND DESIGN APPORACH OF JET ENGINE UNDER DIFFERENT ANALYTICAL PARAMETRIC CONDITIONS. JCR, 7 (17), 3353-3359. doi:10.31838/jcr.07.17.414



Turabian Style

I Venu Gopal. 2020. THERMAL ANALYSIS AND DESIGN APPORACH OF JET ENGINE UNDER DIFFERENT ANALYTICAL PARAMETRIC CONDITIONS. Journal of Critical Reviews, 7 (17), 3353-3359. doi:10.31838/jcr.07.17.414



Chicago Style

I Venu Gopal. "THERMAL ANALYSIS AND DESIGN APPORACH OF JET ENGINE UNDER DIFFERENT ANALYTICAL PARAMETRIC CONDITIONS." Journal of Critical Reviews 7 (2020), 3353-3359. doi:10.31838/jcr.07.17.414



MLA (The Modern Language Association) Style

I Venu Gopal. "THERMAL ANALYSIS AND DESIGN APPORACH OF JET ENGINE UNDER DIFFERENT ANALYTICAL PARAMETRIC CONDITIONS." Journal of Critical Reviews 7.17 (2020), 3353-3359. Print. doi:10.31838/jcr.07.17.414



APA (American Psychological Association) Style

I Venu Gopal (2020) THERMAL ANALYSIS AND DESIGN APPORACH OF JET ENGINE UNDER DIFFERENT ANALYTICAL PARAMETRIC CONDITIONS. Journal of Critical Reviews, 7 (17), 3353-3359. doi:10.31838/jcr.07.17.414