Indian railways mechanical vocational training report 2 haxxo24 i i
1. 2010 INDUSTRIAL TRAINING REPORT
2. ACKNOWLEDGEMENT We take this opportunity to express our sincere gratitude to the peoples who have been helpful in the successful completion of our industrial training and this project. We would like to show our greatest appreciation to the highly esteemed and devoted technical staff, supervisors of the Diesel Loco Shed, Tughlakabad. We are highly indebted to them for their tremendous support and help during the completion of our training ....etc

[:=Read Full Message Here=:]

NO-MOVING-PART
HYBRID-SYNTHETIC JET ACTUATOR
Article Outline
1. Introduction
2. The actuator model
2.1. General
2.2. Amplifier
2.3. Feedback loop
3. Results
3.1. Oscillation frequency
3.2. Modified Strouhal number
3.3. Constant Strouhal number regime
3.4. Constant propagation velocity regime
4. Conclusions
Acknowledgements
References
1. Introduction

Actuators based on the synthetic jet idea are currently becoming of increasing importance for a number of applications, especially involving control of flo ....etc

[:=Read Full Message Here=:]

hello I want some materials for my seminar presentation topic STEAM NOZZLE. Help me find in these topics
....etc

[:=Read Full Message Here=:]

ABSTRACT
In aerodynamics, hypersonic speeds are speeds that are highly supersonic. In the 1970s, the term generally came to refer to speeds of Mach 5 (5 times the speed of sound) and above. The hypersonic regime is a subset of the supersonic regime.
Supersonic airflow is decidedly different from subsonic flow. Nearly everything about the way an aircraft flies changes dramatically as an aircraft accelerates to supersonic speeds. Even with this strong demarcation, there is still some debate as to the definition of superso ....etc

[:=Read Full Message Here=:]

DESIGN OF PRESSURE VESSEL

ABSTRACT
This project work deals with a detailed study and design procedure of pressure vessel. A detailed study of various parts of pressure vessels like shell, closure, support, flanges, nozzles etc. Design is carried according to rules of ASME code section VII, Division I.
The first chapter deals with detailed study of pressure vessel i.e. the various materials used in pressure construction and temperature are mentioned .It also deals with the study of various parts like flanges, support et ....etc

[:=Read Full Message Here=:]

nozzle governing of steam turbine ppt

Governing System

Governor is a heart component of the turbine which controls it during steady state and transient conditions. The governor does this function by controlling the steam flow through the turbine by adjusting the control value. The governor is a control component with advanced protections for the turbine which ensure safe operation of the turbine. Governing system of the turbine does the following functions:



Controls the turbine speed during start-up or in no load condition to permit the u ....etc

[:=Read Full Message Here=:]

In aerospike engine instead of firing the exhaust out of a small hole in the middle of a bell, it is fired along the outside edge of a wedge-shaped protrusion, the spike. The spike forms one side of a virtual bell, with the other side being formed by the outside air . by this design we can over come the demerit of the conventional bell type nozzle (concept of bell nozzle is to efficiently direct the flow of exhaust gases from the rocket engine into one direction. but The exhaust would be a high-temperature mix of gases, has an effectively ran ....etc

[:=Read Full Message Here=:]

In aerospike engine instead of firing the exhaust out of a small hole in the middle of a bell, it is fired along the outside edge of a wedge-shaped protrusion, the spike. The spike forms one side of a virtual bell, with the other side being formed by the outside air . by this design we can over come the demerit of the conventional bell type nozzle (concept of bell nozzle is to efficiently direct the flow of exhaust gases from the rocket engine into one direction. but The exhaust would be a high-temperature mix of gases, has an effectively ran ....etc

[:=Read Full Message Here=:]

I kindly request to give report for seminar presentation
I require all the details.please give me. ....etc

[:=Read Full Message Here=:]

EJECTOR EXPANSION REFRIGERATION CYCLE (EERC)
BY
RAGIL V R
S8, MECHANICAL
S.N.M.I.M.T, MALIANKARA

ABSTRACT
The ejector expansion refrigeration cycle (EERC) is a variant of the standard vapor compression cycle in which an ejector is used to recover part of the work that would otherwise be lost in the expansion valve. In initial testing EERC performance was poor, mainly due to thermodynamic nonequilibrium conditions in the ejector motive nozzle. Modifications were made t ....etc

[:=Read Full Message Here=:]

To get full information or details of aerospike engine please have a look on the pages

http://seminarsprojects.net/Thread-aerospike-engine

if you again feel trouble on aerospike engine please reply in that page and ask specific fields in aerospike engine ....etc

[:=Read Full Message Here=:]

Kindly please send me steam nozzle ppt as free material
with great thanks ....etc

[:=Read Full Message Here=:]

Hi there, I want to give seminar on aerospike nozzles and engines. Can you give the material with which I can give seminar for 15-30 minutes?
[email protected] is my mail id. ....etc

[:=Read Full Message Here=:]

hey man read http://seminarsprojects.net/Thread-DESIGN-OF-PRESSURE-VESSEL-full-report

where detailed material about DESIGN OF PRESSURE VESSEL discussed
and i may republish the content of your material for easy navigation

INTRODUCTION
Definition:
A pressure vessel is a closed container designed to hold gases or liquids at a pressure different from the ambient pressure. The end caps fitted to the cylindrical body are called heads.
The legal definition of pressure vessel varies from country to country, but often involves the maximum safe pr ....etc

[:=Read Full Message Here=:]

1. INTRODUCTION
Rocket engines that work much like an automobile engine are being developed at NASA s Marshall Space Flight Center in Huntsville, Ala. Pulse detonation rocket engines offer a lightweight, low-cost alternative for space transportation. Pulse detonation rocket engine technology is being developed for upper stages that boost satellites to higher orbits. The advanced propulsion technology could also be used for lunar and planetary Landers and excursion vehicles that require throttle contr ....etc

[:=Read Full Message Here=:]

Abrasive Jet Machining
INTRODUCTION
Abrasive water jet machine tools are suddenly being a hit in the market since they are quick to program and could make money on short runs. They are quick to set up, and offer quick turn-around on the machine. They complement existing tools used for either primary or secondary operations and could make parts quickly out of virtually out of any material. One of the major advantage is that they donot heat the material. All sorts of intricate shapes are easy to make. They turns to be a mon ....etc

[:=Read Full Message Here=:]

ABSTRACT

Nowadays concerns about methanol have increased from the viewpoints of environmental protection and versatility of fuels at a global scale. Energetic research on methanol-fueled automobile engines has been forwarded from the viewpoints of low environmental pollution and the use of alternate fuel since the oil crisis, and they are now being tested on vehicles in various countries in the world. Desire for saving of maintenance cost and labour prevails as well as the environmental problems in the field of marine engines. From th ....etc

[:=Read Full Message Here=:]