Tech pedia
creativity, collaboration, compassion



Search Result for Aeronautical Engineering

To Study The Variation Of The Lift & The Drag Coefficient With The Change In The Angle Of Attack For A Naca 0012 Airfoil Profile Used In Wind Rotor Blades And Hence Verify The Experimental Results With The Standard Ones

Taken by :  HARSH SHAH (080410101051) UZAIR MANSURI (080410101017) HARDIK MODI (080410101018) CHINTAN PANDIT (080410101023) NILAY SHAH (080410101052) VISHAL DESAI (080410101008)
College :  SVIT Vasad         Branch:  Aeronautical Engineering
Industry Name: Suzlon Industries limited
Abstract: The project primarily deals with the flow analysis of a 4 – digit NACA airfoil profile which is used in a wind rotor blade. The simulation of the flow over the airfoil will be done using CFX software. The main aim is to study the behavior oflift& drag coefficientsw.r.t. the angle of attack and to find out stable & stalling conditions. Seven different simulations will be carried out for values of angle of attack between -2 degrees to 10 degrees with steps of 2 degrees. The results will then be compared &verified with the standard results. An essential lift to drag coefficient ratio rises with the increase in angle of attack,reaches a maximum value and then starts to fall. The project is based on elements like Flow over an Airfoil, CFD techniques, Wind Blade Aerodynamics & Controls, CFX software & NACA airfoil profile. An introduction to these elements is given in the following pages.

Analysis Of Aerodynamic Characteristics Of External Armour Panels On A Combat Helicopter (ch)

Guide By: Malay Suvagiya
College :  SARDAR VALLABBHAI PATEL INSTITUTE OF TECHNOLOGY, VASAD         Branch:  Aeronautical Engineering
Industry Name: Hindustan Aeronautics Limited
IDP/UDP Field:
Abstract: The report incorporates the Analysis of Aerodynamic Characteristics of External Armour Panels on a Combat Helicopter (CH) Body, performed at RWR&DC (Helicopter Division), Hindustan Aeronautics Ltd. (HAL) - Bangalore. The armour panels are generally attached inside the body, due to spacing constraints panels may not be placed insides the body. In such cases, the armour panels are attached outside the body, which interacts with the airflow, and degrades overall aerodynamic performance of the body. Analysis has been conducted over 6 schemes, (a) Flat Without Gap (b) Flat With Gap (10 mm) (c) With gap (10 mm) Rounded edges (d) With gap (20 mm) Rounded edges (e) Faired Without Gap (f) Faired With Gap (10mm) Variation of lift-drag characteristics and moments has been computed theoretically and computationally for the aforementioned schemes. The aerodynamics effects of rotor, and aerodynamic interaction of attachment used for securing armour panels to the helicopter body have not been considered to reduce the analysis complexity. It has been found that configuration of faired armour panel without gap (case 5) has least drag.

Asset Management System

Taken by :  Disha Patel, Tanvi Patankar, Madhuri Patel, Rucha Patel, Disha Patel, Tanvi Patankar, Madhuri Patel, Rucha Patel
Guide By: Radha teredesai
College :  BABARIA INSTITUTE OF TECHNOLOGY, VADODARA         Branch:  Aeronautical Engineering
Industry Name: Kemrock industries and exports limited
IDP/UDP Field:
Abstract: Now a days asset management system is one of most important web based system for any organization to improve their productivity. This system is to be useful for Kemrock industry. The Asset Management System is a web-based application that was developed using object oriented approach while with c# issued as a programming language, Microsoft SQL server 2008 is for database, Microsoft visual studio 2008 as an editing tool for database. Through the Asset Management System, activities of procurement through management of asset can be administered online which involve user categories such as System Administrator, Super administrator, Regular user and vendor. The amount of information, the complexity of the different new assets and the necessity to increase the productivity, forces portfolio managers to use tools that reduce the work on all these topics. Each asset management department will increase the number of customers that are managed by each employee. Big companies spend millions of Euros developing solutions that try to reproduce the different internal workflows. Asset management is the method that a company uses to track movable assets, for Example factory equipment, desks and chairs, computers. Although the Exact details of the task varies widely from company to company, asset management Often includes tracking the physical location of assets, managing demand for scarce Resources and accounting tasks such as amortization. The term Asset management is used in these guidelines to mean the comprehensive management of asset demand, planning, procurement, operation, maintenance, rehabilitation, disposal and replacement to maximize the overall performance of company. The objective of the dissertation is the development of a software for asset management, also called portfolio management, together with the use of all the tools and techniques that are needed for the development process.

Auto Power Factor Controller

College :  VALIA INSTITUTE OF TECHNOLOGY, BHARUCH         Branch:  Aeronautical Engineering
IDP/UDP Field:
Abstract: This report is established to fulfill the Project requirement for Engineering for V.I.T student, a standard guideline is prepared to standardize various documentations and this report is done mainly to list down all the important aspect of the project or the electrical and electronic device that designed. We introduce a method how to control power factor automatically in the small scale industrial and commercial power supply. As a practical model I design a microcontroller based system. The programming code is developed & used to the microcontroller software developed using high level programming language. In this project we measure the parameter of power factor and calculate the active and reactive power and display on LCD. If the parameter exceeding limit than to give the signal to capacitor bank and it will connect with the supply and solve the problem. As this was my study project I have sincerely tried to develop the concepts.

Civil Unit Booking System

Taken by :  Jitendra R Patel, Jitendra R Patel
Guide By: Niahil Gandhi
College :  SIGMA INSTITUTE OF ENGINEERING, WAGHODIA         Branch:  Aeronautical Engineering
Industry Name: Krishna Infotech
IDP/UDP Field:
Abstract: This is software which has mainly made for civil unit booking system. The software has designed with front –end as VB and back-end as Ms-Access. The current system of the booking of the house or villas or pent house (which will be considered as unit in further pages here in) is manual and is very much messy in case of further reference. The current system is manually operator by various people and integration of the data is not maintained and further data replication is found.As the entries of the booking are done manually by various operators or the owner it is not in the integrated form. The loss of integrity may cause the data redundancy and non-relation of the data while the future use of data is needed. Correct form of calculation is not done and account mess is generated. Manual books are not efficient to maintain the hierarchical structure of the payment structure of the objects and calculative errors are done.

Constructing And Modelling Of A Turbojet Engine With The Most Basic Components To Demonstrate The Working Of A Turbojet Engine

Taken by :  desai fanil nailesh, desai fanil nailesh
Guide By: Mr.M R Mekwan
College :  SARDAR VALLABBHAI PATEL INSTITUTE OF TECHNOLOGY, VASAD         Branch:  Aeronautical Engineering
Industry Name: in house
IDP/UDP Field:
Abstract: The project under the title construction and modelling of a conceptual turbojet engine with the most basic components to demonstrate the working of the engine is braodly classified under six section:- 1. theoritical calculation 2. designing 3. sub-system details 4. drafting 5. operation 6. catia modelling The compressor section is a 2-stage axial type and the turbine is a single stage axial type turbine.the combustion chamber is a singular can annular type with most basic operstion. the pressure output from the two ports at the input of compressor and the outlet of compressor. we feed u-yube manometer to monitor the pressure changes. a thermocouple is fixed in the combustion chamber to keep a tab as the temperature produced in a combution chamber. finally an annemometer is used to measure jet exit velocity, with these parameters, we can explain the operation of the engine which is exemplified in the pressure and temperature reading(variation). Starter mechanism is quite well explained in this report and its function and significance in who dealt with due consideration in the report

Engine Plates Controller

Taken by :  Desai Nileshwari, Desai Nileshwari
Guide By: Hemanshu Rana
College :  MAHATAMA GANDHI INST. OF TECH., EDUCATION & RESEARCH, NAVASARI         Branch:  Aeronautical Engineering
Industry Name: L&T
IDP/UDP Field:
Abstract: this will make the engine plates controll automatic by using computer controll

Enterprise Information Portal

Taken by :  Kamani Rashmi Vijaybhai, Shah Virti Dharnendrakumar, Thakkar Digna Sureshbhai, Kamani Rashmi Vijaybhai, Shah Virti Dharnendrakumar, Thakkar Digna Sureshbhai
Guide By: Tushar J. Raval
College :  GOVERNMENT ENGINEERING COLLEGE, PATA         Branch:  Aeronautical Engineering
Industry Name: Bhasjaracharya Institute Of Space Application And Geology
IDP/UDP Field:
Abstract: We have implemented a Enterprise Resource Portal. We worked together for 1 year at BISAG.

Fin Fan Water Cooling System Using Plc And Scada

Taken by :  Rustagi Palak Pradeep, Rini Sharma, Rustagi Palak Pradeep, Rini Sharma
Guide By: Mr. C P Vaishnav
College :  S. P. B. PATEL ENGINEERING COLLEGE, MEHSANA         Branch:  Aeronautical Engineering
Industry Name: Satyam Industries
IDP/UDP Field:
Abstract: Abstract (ii) This project is based on heat exchanging through a Fin Fan Water Cooling System using PLC and SCADA. The company we visited operated the fin fan cooling system manually. The problems faced by manual operation are that twenty-four hour manual supervision is required and the accuracy of the desired temperature is also not maintained. The manual operation is very time consuming and it is also not cost efficient in the long run. Moreover, the debugging of the system becomes very difficult if a fault occurs in any fan or any component of the system. To solve this problem, we decided to use PLC and SCADA to operate the system. Through PLC programming, one can program the desired functionality of the system and can rely on it as it is computerized, hence does not make any mistakes. Also, with SCADA, we can eliminate the need for site visits by the personnel for inspection, adjustments and data collection. SCADA software enables one to monitor the system in real time. Hence, we have incorporated the use of PLC and SCADA in our project. The cooling system runs entirely through PLC programming and the graphical representation of the system can be viewed in real time in the SCADA screen. We can not only view the real time trends but can also control the working of the fans from our desktop through the SCADA software. The initial cost of PLC and installing the SCADA software is high but in the long run, it proves to be very cost efficient ant time efficient. Moreover, the entire system can be checked and tested as and when required.

Gsm Operated Induction Melting Machine

Guide By: Hardik Patel
College :  NARNARAYAN SHASTRI INSTITUTE OF TECHNOLOGY, JETALPUR         Branch:  Aeronautical Engineering
Industry Name: Oritech Solution
IDP/UDP Field:
Abstract: • Induction Melting Machine whenever any information is required, worker has to take reading of running process every time. This process is very much time consuming and also waste of paper work. There is a requirement that to improve in the system design. So our project is particular on this application that provides all the useful information and, there is less time consume. .So here our IDP gives solution for here’s problem GSM Operated Induction Machine provides much more features. • GSM – Global System for Mobile Communication is used as a media which is used to control and monitor the industrial equipments from anywhere by sending a message. It has its own deterministic character. Thereby, here GSM is used to monitor and control the DC motor, Stepper motor, Temperature sensor and Solid State Relay by sending a message through GSM modem. Hence no need to waste time by manual operation and transportation. • The aim of the project is to develop a system, which uses Mobile technology that keeps control of the various units of the Induction Melting Machine, which executes with respect to the signal sent by the mobile. • GSM Operated Induction Melting Machine plays a very important role. The ease of operation of the kit and low cost add up as an additional advantage for its usage We have designed our kit using 89V52 micro controller which is itself very reliable and also operates very efficiently under normal condition. • The design is implemented at a very economical price. The total cost incurred by us in designing this kit is very less and further we have developed the GSM operated induction melting machine which is more economical rather than just interfacing those which are readily available in the market.

Hybrid Wind-solar Power Production

College :  G. H. PATEL COLLEGE OF ENGINEERING & TECHNOLOGY , V.V.NAGAR         Branch:  Aeronautical Engineering
IDP/UDP Field:
Abstract: Our Project Deals with Wind and Solar Energy and Controlling them with use of Micro-Controller or Other Electronic Circuit. In this system the windmill and a solar panel will be simultaneously mounted on a pole and the pole will inturn be mounted at a place where the solar radiations and wind speed will be sufficient. A controller or PLC circuit can be mounted on the pole. The controller/PLC will work as a switch to deliver power from windmill as well as from solar panel. When solar energy is not available, it will switch over to windmill and vice versa. We are working on a small wind-solar hybrid system which is able to generate power in few watts but by making small changes it can be applicable to even big wind-solar hybrid system. By using this concept we can generate power in Mega-Watts in future, Conventional resources can be preserved and free energy which is available in form of wind and light can be used effectively. This is very futuristic concept as lot of green energy production can be encouraged with the help of this hybrid system and very small space of installation is required. This also reduces the cost of production and the power will be generated round the clock.

Instance Bluetooth Messenger

Taken by :  Jamariya Raju Karabhai, Jamariya Raju Karabhai
Guide By: Dhara Bush
College :  GOVERNMENT ENGINEERING COLLEGE ,RAJKOT         Branch:  Aeronautical Engineering
Industry Name: Aarya Technologies
IDP/UDP Field:
Abstract: This work contains research in usage of Bluetooth applications for mobile device. In addition a detailed exploration of Bluetooth and J2ME the work consist of design and implementation of sample application using Bluetooth transfer called Instant Bluetooth Messenger (IBM).This application servers as a communication platform, enabling two or more BT clients to connect their mobile phones and send each other text messages. Create a much more comprehensive chat system containing Rooms, user groups, multimedia data, encryption of messages, etc.

Mi-card Reader Using Rabbit Processor

Guide By: Mr.Swarup Pal
College :  BABARIA INSTITUTE OF TECHNOLOGY, VADODARA         Branch:  Aeronautical Engineering
IDP/UDP Field:
Abstract: It is prototype of taking ticket automatically at one station. Our whole project is completed by Rabbit processor and mi-fare card.We take this idea after visiting Delhi metro Train. our project will be applicable for city bus system.

Netbios Enumerator

Guide By: Purvik Rana
College :  VALIA INSTITUTE OF TECHNOLOGY, BHARUCH         Branch:  Aeronautical Engineering
Industry Name: MAGNETS POWER
IDP/UDP Field:
Abstract: In our project we make a utility which is useful for network user to get the resources and information from the systems that connected in the network. By using this software user can monitoring the systems for the available resources and perform the operation on particular system. This tool mostly used by the network administrator to monitor the network systems by scanning the systems. This tool is very handy and simple to use. All we need to do is to provide the IP address range. This tool will search for the available resources and other information from the target system one by one. The output is displayed in the tree structure so that user can easily view the information he got as a result of scanning.

Numerical Analysis Of A Generic Missile With Different Grid Fin Configurations And Their Comparison For Optimum Performance

Taken by :  Harsh Shah, Chirag Sheth, Vishal Desai, Harsh Shah, Chirag Sheth, Vishal Desai
Guide By: Malay Suvagiya
College :  SARDAR VALLABBHAI PATEL INSTITUTE OF TECHNOLOGY, VASAD         Branch:  Aeronautical Engineering
Industry Name: In-House
IDP/UDP Field:
Abstract: A lattice grid fin is an unconventional missile control surface with an outer frame supported by an internal lattice grid of lifting surfaces. The project focuses on transonic analysis of the missile with different grid fins. An important aspect was to determine the critical mach no. where the flow gets choked. Another aspect was to find out the aerodynamic coefficients including lift, drag and pitching moment coefficients. The variation of these coefficients with angle of attack at different mach nos. has been studied. Three different grid fin configurations have been studied for their aerodynamic characteristics. They are baseline, AFIT and coarse configurations. They differ by their web thickness and the number of webs. Another configuration, that of a planar fin has also been studied. A comparison of the aerodynamic characteristics of all these configurations has been made. Also, the flow field for each configuration has been captured. The variations that have been studied at different mach nos. are normal force coefficient with respect to angle of attack, axial force coefficient with respect to angle of attack and pitching moment coefficient with respect to angle of attack.

Regarding Higher Gas Consumption, Lower Production Cycle In Kiln & Various Defects In Floor Tiles

Guide By: Assi. prof, PARESH K. KASUNDRA
College :  B. H. GARDI COLLEGE OF ENGINEERING & TECHNOLOGY, KALAWAD         Branch:  Aeronautical Engineering
IDP/UDP Field:
Abstract: Shapphire ceramics is one of the renowned industry in making floor tiles. In shapphire ceramic pvt. Ltd. Company is having machinery like spredryer, boil mill, hydraulic press & kiln. All of the above the main and is of most important part is kiln. Kiln is a thermally insulated chamber, or oven, in which a controlled temperature regime is produced. It has become the prime importance that guidelines are being needed for safe, efficient, inexpensive kiln. This report shows various components of kiln as well as the problems that are occurred in it. In addition with that this report also shows the detail description of the various problems occurring in it. Some of the stages that are responsible for making floor tiles are also being mentioned in this particular report.

Smart & Secure Trafic Monitoring System

Guide By: kaushal P. makhecha
College :  L. D. R. P. INSTITUTE OF TECHNOLOGY, GANDHINAGAR         Branch:  Aeronautical Engineering
Industry Name: Doordarshan kendra, Ahmedabad
IDP/UDP Field:
Abstract: Introduction: We are having a project on Smart & Secure Traffic Monitoring System at Doordarshan Ken-dra, Ahmedabad. In this project we are going to study in detail about traffic security &monitoring and make a model of traffic monitoring system and performance evolution of digital access technology. Working: By using the various components GSM, RFID, Pen camera, resisters, capacitors, microcon-troller and IC’s, we are going to implement traffic monitoring system hardware with using different type of software. Objective: • The detail study of traffic monitoring system technology. • The designing model of traffic monitoring system. • The performance evolution; RFID maintenance & TMS. Expected Result: If this project will work than, we can connect the traffic monitoring system to a rural as well as urban area and checkout all the objectives. Key words: • TCS means Traffic Monitoring System. • RFID means Radio-frequency identification.

Study Of Morphing Concept

Taken by :  Jinita Desai, Devesh Chadha, Jinita Desai, Devesh Chadha
Guide By: Malay Suvagiya
College :  SARDAR VALLABBHAI PATEL INSTITUTE OF TECHNOLOGY, VASAD         Branch:  Aeronautical Engineering
Industry Name: Suzlon Energy Limited, Vadodara
IDP/UDP Field:
Abstract: Aircrafts are becoming smaller, lighter, and more flexible, while their performance requirements are becoming more stringent. This is especially true for Uninhabited Combat Air Vehicles (UCAV) or Micro Air Vehicles (MAV). These vehicles operate at relatively very low Reynolds Number which revived the research on the performance of airfoils at relatively low Reynolds Numbers. There are many problems with the application of low Reynolds Number out of which the most inevitable is flow separation. In order to overcome this effect, there are some changes required to get the required performance characteristics. This phenomenon is called MORPHING and the concept is called MORPHING CONCEPT. In this project the general effects on performance of several general characteristics of Two-Dimensional NACA 0015 Airfoil are explored by variations in Thickness and Camber. The velocity of free stream considered for the study is 100 km/hr and 120 km/hr which correspond to Re 104 with the angle of attack varying from zero lift angle to stall angle. The analysis of the characteristics is done in FLUENT. In the analysis part, first the construction of the airfoils by varying the camber and thickness are constructed and the tetra-hedral meshing is done in GAMBIT. Then the boundary conditions of velocity inlet and pressure outlet with standard K-? model are set for the computational analysis in FLUENT. By implementation of various changes, computational results indicate that the detailed section geometry has a profound effect on airfoil performance. Improved section performance requires that camber should be high to get better performance and delay of the flow separation. Also the overall thickness should be minimized to overcome the drag penalty of the high thickness.

Testing Of Cables & Conductor

Taken by :  Chaudhari Kunal Govindbhai, Lodhiya Yash Piyushbhai, Mothaliya Ashishkumar Amrutlal, Chaudhari Kunal Govindbhai, Lodhiya Yash Piyushbhai, Mothaliya Ashishkumar Amrutlal
Guide By: Mr. Maulik C. Pandya
College :  L. D. R. P. INSTITUTE OF TECHNOLOGY, GANDHINAGAR         Branch:  Aeronautical Engineering
Industry Name: Sabar Cables PVT LTD
IDP/UDP Field:
Abstract: This project involves the study of Testing of Cables and Conductors. In the study, it is very much necessary to get knowledge of practical point of view. So industrial training is the part of our study. We have compiled our training at SABAR CABLES PVT LTD. By industrial training we learn many practical aspects. During the training we tried to get maximum information for related topic and we have prepared a project report on industrial training. This project is an attempt to make practical studies about the Testing of Cables and Conductor. Testing being one of the important steps of any designing, our attempt includes the tests carried on the cables and conductors. These tests are also compared to the respective I.S.

To Increase The Efficiency Of Condenser By Removing Scaling Formation For Condenser Tube

Taken by :  Rushabh m Champaneri, Ravi h dabla, Rushabh m Champaneri, Ravi h dabla
Guide By: prof. n. j. patel
College :  SHRI C. U. SHAH COLLEGE OF ENGINEERING & TECHNOLOGY, WADHWA         Branch:  Aeronautical Engineering
Industry Name: G.S.E.C.L
IDP/UDP Field:
Abstract: Abstract Generally the condenser is used to change the phase of water to convert it from vapor to liquid form. The water is generally used in condenser for cooling purpose. Generally they used simple water as cooling water because mineral water becomes quite costly as cooling water so simple water is being used in condenser as cooling water. So due to all this impurities the different types of fouling takes place inside the condenser tubes like fouling, chemical fouling etc. Due to that fouling the heat transfer rate between this fluids not occurring according to design of condenser. So the efficiency becomes low and we are unable to catch the desired output. So renovation of fouling from the condenser tubes is very essential to get the desired output. So there are different methods like water jetting, acid cleaning, bullet cleaning, sponge ball cleaning are used to remove the fouling. The selection of method for cleaning condenser tube is based on fouling takes place inside the condenser tubes.

Total : 30

1 2

News & Announcement

View All  

Message of Appreciation

I am extremely happy to see an initiative of SRISTI (Society for Research and Initiatives for Sustainable Technologies and Institutions...
By Dr. A.P.J. Abdul Kalam

read more  


Techpedia - Peru

Follow Us

© 2014 TechPedia, all rights reserved