4th International Conference Emerging Trends in Mechanical Science (ICEMS-2018)
(Volume-1)

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Title
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Effect of High-Lift Devices on Aircraft Wing
Country
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India
Authors
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Gaurav B. Mungekar || Swapnil N. More || Samadhan V. Niwate || Prof. Sagar Dharmdhikari
Page
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01-05

In aircraft design, a high-lift device is a component on an aircraft's wing that increases the amount of lift produced by the wing. Wind tunnel test is a common method for wing analysis, but the problem with wind tunnel tests is that they are expensive and time consuming. A simple designed wing geometry was analyzed and modified by adding different high-life devices, further analysis was carried out on the modified wing for a comparative study. For this purpose, a virtual wind tunnel model was created and CFD analysis was carried out at various angle of attacks for each wing geometry separately. The lift and drag forces and coefficients of each wing were determined and the comparative study of these showed how minute changes to the wing improves its overall flow characteristics.

 

Keywords: - Angle of attack, CFD analysis, Flaps, Lift, Simulation

[1] Shreyas Krishnamurthy, Suraj Jayashankar, Sharath V. Rao, Rochen Krishna T S, Shankargoud Nyamannavar, "CFD Analysis Of An RC Aircraft Wing", International Journal of Mechanical And Production Engineering, Volume- 2, Issue-9, Sept.-2014
[2] Shivasharanayya Hiremath, Anandkumar.S.Malipatil, "CFD Simulations of Aircraft Body with Different Angle of Attack and
Velocity", International Journal of Innovative Research in Science,Engineering and Technology, Vol. 3, Issue 10, October 2014

 

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Title
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Mechanical Characterisation of Kenaf Fibre Reinforced Polymer Matrix Composite for Automotive Sector
Country
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india
Authors
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Anand Kamble || Santosh S Bagewadi || Morrish Kumar
Page
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06-10

The manmade fibre reinforced composites are costlier, may affect environment, and the scrap produced during fabrication is not reusable. Hence to overcome this we have decided to replace synthetic fibre to natural fibre. The natural fibre selected for present work is kenaf fibre. The present work investigates the strength of kenaf fibre reinforced composite for different proportions of matrix, fibre and filler materials. Experimental investigations are carried out in order to determine mechanical properties by tensile test and bending test. According to ASTM standards specimens are prepared and the results are validated through ANSYS. The specimens were prepared with varying resin 30%, 35% and 40% for specimen A, B and C respectively. This present work contributes for development and characterization of kenaf fibre reinforced composite for Bus Body building activities.


Keywords: - ANSYS, Kenaf fibre, polymer matrix.

[1]. H.M. Akil, M.F. Omar, S. Safiee, Z.A.M. Ishak, A. Abu Bakar, A.A.M. Mazuki "Kenaf fibre reinforced composites A review"
Materials and Design 32-2011-4107–4121.
[2]. B.F. Yousif, A. Shalwan, C.W. Chin, K.C. Ming "Flexural properties of treated and untreated kenaf/epoxy composites" Materials and Design 40 -2012- 378–385.
[3]. A.Elsaid, M. Dawood, R. Seracino, C. Bobko, "Mechanical properties of kenaf fibre reinforced concrete" Construction and
Building Materials 25-2011-1991–2001.
[4]. N. Saba, M.T. Paridah, M. Jawaid "Mechanical properties of kenaf fibre reinforced polymer composite: A review" Construction and Building Materials 76 -2015- 87–96.
[5]. Takashi Nishino, Koichi Hirao, Masaru Kotera, "Kenaf reinforced biodegradable composite" Composites Science and Technology 63-2003-1281–1286.

 

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Title
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Review on Electro Discharge Machine [EDM] and Ultrasonic Assisted Electro Discharge Machine [USA-EDM]
Country
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India
Authors
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Atish B. Mane || Dr. Pradeep V. Jadhav
Page
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11-14

Electrical Discharge Machining (EDM) is a non-traditional machining process used for machining of hard materials. EDM processes are used for cavity machining, producing dies and molds, and intricate machining operations in hard, difficult to machine. In recent years, researchers focused to improve the process performance of EDM processes. This paper reviews the research work carried out by the researchers on EDM andon vibration assisted EDM. The review of this research work enables the better understanding of the vibration assisted EDM process. This study also discusses the influence of vibration parameters such as vibration frequency and amplitude on the MRR, EWR, and surface roughness. The research gap in the respective area of research are also presented in this paper.

 

Keywords: - USA-EDM, Work piece vibration, Tool vibration, MRR, EWR, Surface roughness

[1]. K.M Patel, Pulak M. Pandey . P VnkateswaraRao, Optimization of process parameters for Multi- performance characteristics in EDM of AL2O3 ceramic composite, Int J Adv Manuf Technol, 2010, pp. 1137-1147.
[2]. Azizul Bin Mohamad, Arshad Noor, Siddiquee, Gulam Abdul Quadir, Zahid A. Khan, V.K. Saini , Optimization of EDM process
parameters using Taguchi method, International Conference on Applications and Design in Mechanical Engineering ,2012.
[3]. E. Aliakbari& H. Baseri, Optimization of machining parameters in rotary EDM process by using the Taguchi method, Int J Adv Manuf Technol, 2012, pp. 1041-1053.
[4]. S. Singh, Optimization of machining characteristics in electric discharge machining of 6061Al/Al2O3p/20P composites by grey relational analysis, Int J AdvManuf Technol, 2012, pp. 1191- 1202.
[5]. Sushil Kumar Choudhary, Dr. R.S Jadoun, Current Advanced Research Development of Electric Discharge Machining (EDM): A Review, International Journal of Research in Advent Technology, 2014, pp. 273-297.

 

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Title
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Optimization of Fuel Nozzles for Maximum Thrust using Multi-Disciplinary Optimization
Country
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India
Authors
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Gowtham Dronamraju || Prof. Daksheeswara Reddy Chamala
Page
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15-20

Nozzles of various sizes and geometries are being used in various fields of engineering. A nozzle is a mechanical device used to convert chemical, thermal energy into kinetic energy. It converts low velocity, high pressure & high temperature gas into high velocity at the exit. It is basically a device used to control rate of flow, speed, direction, mass, shape and/or pressure of the fluid across a system. In an automobile, a nozzle is used to spray fuel air mixture to the piston cylinder through carburetor. A convergent- divergent nozzle is a most commonly used nozzle in aerospace and automobile industries. In this project, diesel and gasoline engine nozzlesare modeled to optimize for maximum performance using multidisciplinary optimization technique................

 

Keywords - Convergent-Divergent Nozzle, Multi-Disciplinary optimization, Structural analysis, Mass flow rate.

[1]. OB Zimmerman, "IC Engines and their tractors", Forgotten Books Publishing, pp 493-494, 1988.
[2]. Robert Bosch, "Distributor Type Diesel Fuel Injection Pumps: Bosch Technical Instruction", Bosch GmbH, p23-71, 2003.
[3]. Challen, "Diesel Engine Reference Book" Reed Educational and Professional Publishing Ltd., Second Edition, pp.260-301, 1999.
[4]. Lei Liu et al, "Analysis and Design of the System for Detecting Fuel Economy"IEEE. 2010 International Symposium on
Intelligence Information Processing and Trusted Computing, 28-29 Oct. 2010.
[5]. Rajendran, S & Purushothaman, K. (2014). Analysis of fuel flow in internal combustion engine using -CFD. International Review of Mechanical Engineering. 8. p480-487.

 

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Title
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Estimation of Angle of Attack on a Fighter Aircraft During Its Avionics Upgrade
Country
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India
Authors
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Ajai Kumar Rai
Page
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21-25

This paper presents a scheme for estimation of angle of attack (AOA) and angle of side slip (AOS) on a fighter aircraft during its avionics upgrade. The scheme was implemented and validated on a fighter aircraft designed and developed in early 1970 which was required to undergo major avionics upgrade to enhance its operational capabilities with modern sensors and avionics systems. The original version of the aircraft hadmechanical AOA which was not reliable and accurate to meet the combat performance (ground attack role) expected from the upgraded version of the aircraft. A scheme was developed for inflight estimation of AOA using inertial sensor data from the Inertial Navigation System having Laser Gyros.............

 

Keywords -Inertial navigation system(INS), Kalman filter, Angle of attack, Stability matrix, Control matrix, Euler angle

[1]. G K Singh, Pratima and Shyam Chetty, Evaluation of Inertial/ISU based AOA estimation schemes, TM NO: SWS/TM/003, Dec 2000.
[2]. Candy JV, signal processing: The Model Based approach, McGraw Hill International Edition, Singapore, 1987.
[3]. Brain L. Stevens &Frank L. Lewis, Aircraft control and Simulation, A Wiley-Interscience Publication, 1992
[4]. Robert C Nelson, Flight Stability &Automatic Control, Mcgraw-Hill international second edition, 1998
[5]. Joseph E. Zeis, JR, Captain, USAF AFIT/GAE/AA/88 J-2 Jun 1988, Thesis on angle of attack & side slip estimation.
[6]. N Shantha Kumar, Girija G, Filtering & Fusion based reconstruction of Angle of Attack, National Conference on range technology (NACORT) 2006- ITR, Chandpur

 

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Title
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Experimental Study On Electro-Discharge Machining Of Oxygen Free Copper Cu102 For The Application Of Beam Dump
Country
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India
Authors
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Amit Motwani || Y.M.Puri
Page
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26-30

An experimental study on the effects of electro-discharge machining (EDM) parameters on the surface finish and material removal rate (MRR) by machining copper work piece with copper electrode is presented. The varying significant parameters are discharge current, pulse on-time and pulse off-time and other parameters such as gap voltage, duty cycle, polarity, flushing pressure etc. are kept constant for the proposed machining. In this all factorial combinations were used for getting the optimum parameters for the required average surface roughnessRa of less than 1μm for the application of finishing a copper beam dump.

 


Key words: - ANOVA, Copper, EDM, Regression, Surface roughness.

[1] J Jeevamalar,Ramabalan,Die Sinking EDM Process Parameters:A Review, Int. J. Mech. Eng. & Rob. Res. Vol. 4, No. 1, January 2015.
[2] Y.S. Wong , L.C. Lim, IqbalRahuman, W.M. Tee, Near-mirror-finish phenomenon in EDM using powder-mixed dielectric, Journal of Materials Processing Technology 79,1998, 30–40.
[3] Amit Kumar, AmitavaMandal, AmitRai Dixit, RachitRanjan, Comparison of Surface Roughness and Material Removal Rate in Die Sink EDM using Deionized Water and Powder Mixed EDM as a Dielectric Medium, Proceedings of 6th International & 27th All India Manufacturing Technology, Design and Research Conference, 2016.
[4] H.K. Kansal, Sehijpal Singh , P. Kumar, Parametric optimization of powder mixed electrical discharge machining by response surface methodology, Journal of Materials Processing Technology 169,2005, 427–436.
[5] Y. C. Lin,B. H. Yan, F. Y. Huang, Surface Improvement Using a Combination of Electrical Discharge Machining with Ball Burnish Machining Based on the Taguchi Method, Int J AdvManufTechnol 18, 2001, 673–682.

 

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Title
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Study and Analysis of Automobile Suspension System using Bond Graph Technique
Country
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Iran
Authors
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Rahul Y. Girase || Dr. Animesh Chatterjee
Page
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31-36

In this paper Bond Graph based approach is used for the Design and Analysis of suspension system. The suspension model used for analysis is "Two degree of freedom Quarter car model‟ and the controller use is PID Controller. The response of the system is simulated by using the software "Symbol‟s Shakti".Basically, the automobile suspension‟s design incorporates two criteria‟s which are road handling (Safety factor) and passenger comfort. In order to improve the ride comfort and stability by reducing the body acceleration in vehicles caused by the road irregularities, suspension system plays an imperative role in retaining the continuous road wheel contact for better road holding............

 

Keywords - Quarter Car model, Bond Graph Modeling, PID Controller etc.

[1]. A S. Emam , Fuzzy Self Tuning of PID Controller for Active Suspension System, Advances in Powertrains and Automotives, 2015, Vol. 1, No. 1, PP 34-4
[2]. Amalendu Mukherjee, Ranjit Karmakar, Modelling and Simulation of Engineering Systems through Bondgraphs (Narosa
publications ISBN 81-7319-279-0).
[3]. Priti Tiwari, Dr.G.R.Mishra, Simulation of Quarter Car Model, IOSR Journal of Mechanical Engineering, 2014, PP 85-88.
[4]. Rijumon K , Murtaza M A, Ajith Krishnan, A Comparison between passive & semi active suspension systems. International Journal of Innovative Research in Science, Engineering and Technology Vol. 2, June 2013, ISSN: 2319-8753, PP 2412-2416
[5]. Nitish Katal, Sanjay Kr. Singh, Optimization of PID Controller for Quarter-Car Suspension System using Genetic Algorithm,
International Journal of Advanced Research in Computer Engineering & Technology, Volume 1, Issue 7, September 2012.
[6]. Y. Liu, T.P. Waters, M.J. Brennan ,A comparison of semi-active damping control strategies for vibration isolation of harmonic
disturbances. Journal of Sound and Vibration 2005,280, PP 21-39.

 

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Title
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Design And Analysis On Aircraft Wing To Fuselage Lug Attachment
Country
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India
Authors
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Madiha Khan || Mohammed Rehman Khan || D. Smitha
Page
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37-42

There are two classes of loads which acts on the aircrafts which are surface forces and body forces. Surface forces include aerodynamic and hydrostatic pressure forces while body forces are due to gravitational and inertial effects on the volume of the structure of an aircraft. In these aerodynamic forces are more severe. With the pressure load which occurs due to the production of lift force, bending moment and shear forces will be acting on the wing. These are the most important cases of forces while studying about the Wing to Fuselage lug attachment connections. Rarely an aircraft will fail due to a static overload during its service life. For the continued airworthiness of an aircraft during its entire economic service life, fatigue and damage tolerance design, analysis, testing and service experience correlation play a pivotal role...............


Keywords – Wing to fuselage lug attachment, stress concentration, Fatigue life, S-N data, Factor of safety, Occurrence, Exceedence and Damage tolerance

[1] IJSRD - International Journal for Scientific Research & Development| Vol. 4, Issue 12, 2017 |
[2] IJMETMR –International Journal and Magazine of Engineering and Technology, Management and Research | vol. 4, august 2017|
[3] International Journal of Engineering Research and General Science Volume 4, Issue 1, January-February, 2016
[4] O. Gencoz, U.G. Goranson and R.R. Merrill, ―Application of finite element analysis techniques for predicting crack propagation in lugs‖.Boeing Commercial Airplane Company, Seattle, Washington, 98124, USA.

 

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Title
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Fracture, Fatiuge Growth Rate And Vibration Analysis Of Cam Shafts Used In Railways
Country
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India
Authors
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Marla Srikanth || D Venkata Subbarao
Page
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43-46

The cam shaft and its combined capacity guide the beginning and finish of the two valves. The associated parts are thrust rods, rocker arms, valve springs and tappets. It consists in of a cylindroids oppression continuous over the number of extend lobes extend from it, one for each gate. A camshaft is a shaft to which a cam is undisturbed or which a cam shapes a component part. The vibration in the camshaft reduces the effectiveness of the engine and augments the rubbing between the rocker arms and the camshaft. This study is centered towards the oscillation analysis of the variegated camshafts that are used in times and to find a material that have the minimum native crowd and no effects on the ability of the electrical engine. The goal of the project is to design cam shaft analytically, its modeling and Analysis under FEA.............

 

Keywords - Camshaft, CREO, FEA, Fracture, Fatigue, Model analysis.

[1]. A.S.Dhavale, V.R.Muttagi "Study of Modeling and Fracture Analysis of Camshaft" International Journal of Engineering Research and Applications, Vol. 2, Issue 6, November-December 2012, pp.835-842.
[2]. Mahesh R. Mali, Prabhakar D. Maskar, Shravan H. Gawande, Jay S. Bagi , " Design Optimization of Cam & Follower Mechanis of an Internal Combustion Engine for Improving the Engine Efficiency", Modern Mechanical Engineering, 2012, 2, pp.114-119
[3]. Bayrakceken H, Ucun I. & Tasgetiren S. "Fracture analysis of a camshaft made from nodular cast iron". [ 1240-1245] 3 NOV 2005.

[4]. Paradon V. "An Impact Model for Industrial CamFollower System: Simulation And Experiment". [ 01-11] 11th OCT, 2007
[5]. G.K. Matthew., D. Tesar.(1976), Cam system design: The dynamic synthesis and analysis of the one degree of freedom model, Mechanism and Machine Theory, Volume 11, Issue 4, Pages 247-257.