Evaluation And Constant Motivation Towards Carrying Out The Tasks

As a result of the experiment and computation of data, the aerofoil was found to have a critical Mach number of M=0.732. Below this freestream Mach number the Prandtl-Glauert law predicted results very

I am Prathyusha Velthuri bearing Id 700629725.This is my Second Report on my Internship in CS (5020).

I am writing to express my keen interest in your level two internship at the Urgent Care in High Desert Regional Health Center. I discovered this site while job shadowing and really liked the friendly, working environment. I believe that my patient assessment skills, dedication, and hard working habits make me an excellent candidate for the position.

This memo describes my progress to date in the course COSC 684 300: Professional Internship in Summer 2015 semester. I shall also discuss my plans to successfully complete the course in August 2015. The memorandum would be divided in three main task areas which were agreed at the time of the individual internship agreement between me and the department.

Thank you for offering me the position of Human Resources Undergraduate Program Intern at Cisco. I am truly grateful for the time you took to interview me, and how courteous you have been throughout this entire process.

This internship will gain me some experience of working in a collaborative environment with engineers as well as programmers. The tasks are related to the areas of my knowledge and interests. Overall, it’s a great opportunity for me to get my foot in the door of a cooperate world.

The field of Information technology has been around for quite some time now. The field has matured and is now able to handle the millions of users that interact with various businesses or governments through their websites. I am applying for the city of Boca Raton Internship in Information Technology because I want a career in web and network functions. I believe the Information Technology internship as it applies in government setting will be invaluable to me in gaining experience .

The Lift Coefficient CL is calculated using the graphs 1-6. In this report counting the squares method is used to calculate the area between the curves for pressure distribution on the upper surface and lower surface. The area gives the lift coefficient at particular angles

Ever since I was little I was amazed at the ability for a machine to fly. I have always wanted to explore ideas of flight and be able to actually fly. I think I may have found my childhood fantasy in the world of aeronautical engineering. The object of my paper is to give me more insight on my future career as an aeronautical engineer. This paper was also to give me ideas of the physics of flight and be to apply those physics of flight to compete in a high school competition.

I take this opportunity to express my sincere thanks and deep gratitude to all those people who extended their whole hearted co-operation and have helped me in completing this project successfully.

-The protractor of the aerofoil connected to the lift and drag voltmeters was then used to vary the aerofoil’s angle of attack from 0° to 20°. Lift and Drag voltage values measured for each angle were recorded and calibration coefficients of 6.7 and 6.4 were used to obtain force Newton values for lift and drag. The lift and drag forces obtained for each angle were then plugged into equations (3) and (4) to obtain lift and drag coefficients. Equation (5) was used to calculate a theoretical value for the lift coefficient.

Since the beginning of recorded history, humans have always had a fascination with flight. Now that we live in a world where boarding an airplane and flying across the country – or even the world - is simply a part of everyday life, the wonder of flight has diminished for many. Despite this, physics students from all around continue to delight in the many physical forces that play a part in keeping these huge objects (like jumbo jets) from falling out of the sky!

In the end I would like to extend my regards to the Head of the Department Dr.Deepak Arora for giving me the opportunity to present my term paper under the guidance of Dr Deepshikha Agarwal.

The aerodynamic characteristics of a Circulation Control Wing (CCW) air foil have been investigated and comparison studies were made by different companies and aeronautic organization throughout world. The program has been very intense and many original results have been granted though different models of Circulation Control Wings. CCW system as tested will be difficult without examining the noise field of an isolated thin slot of span comparable to that used in the CCW itself. Moreover, many more work has been done like extremely high aspect ratio jets similar to the CCW slot. This technology mainly use on the main wing of an aircraft in order to increase the maximum lift coefficient when large lifting forces at low speeds. The implementation of CCW system can create more air flow over the surface of flaps and slates consequently aircrafts can allow much more lift at low speeds.

Acknowledgments It is necessary to know the relevance between theoretical and practical knowledge. So a student can only claim himself as a student of true knowledge by virtue of preparing such kind of internship report. It is time to thank all who helped me to complete this project successfully. First of all, I offer my heartfelt gratitude and thanks to Almighty Allah who has given me the learning power in the earth. Shibli Noman Khan, School of Business, Independent University Bangladesh, is my academic supervisor. I am grateful to him for the flexibility in the work scope he provided me. His encouragement and advice worked as a foundation stone for this report. I convey my gratitude for his time and continuous support. Mr. Uzzal Kumar