Unsteadiness in aircraft design
A Report
On
UNSTEADINESS IN AIRCRAFT DESIGN
By
AVIRAL TALWAR
2011A4PS152U
At
BITS Pilani Dubai Campus
Dubai International Academic City, Dubai
U.A.E
Second Semester, 2013-2014
A Report
On
UNSTEADINESS IN AIRCRAFT DESIGN
BY
AVIRAL TALWAR
2011A4PS152U
Prepared in Partial Fulfillment of the
Project Course: ME F366 Laboratory Project
At
BITS Pilani Dubai Campus
Dubai International Academic City, Dubai
UAE
Second Semester, 2013-2014
II
MECH
BITS Pilani, Dubai Campus
Dubai International Academic City, Dubai
UAE
Course name: Laboratory Project
Course number: ME F366
Duration: 23.02.2014 to 22.05.2014
Date of start: 23.02.2013
Date of submission: 22.05.2014
Title of Report: Unsteadiness in aircraft design
Name / ID Number: Aviral Talwar/ 2011A4PS152U
Discipline of Student: B.E (Hons) Mechanical Engineering
Name of Project Supervisor: Dr. A.M. Surendra kumar
Project Area: Aerodynamics, Fluid Dynamics, Elasticity
Abstract:
The traditional process of aerodynamic design is carried out manually by trial-and-error method. This process requires a large number of design engineers working alongside a huge budget. In order to overcome this manual method, the technologically driven software design using CFD will provide a cost effective optimal design method.
Software products for automatic aerodynamic design are intended to solve the basic problem of preliminary aerodynamic design: to develop a configuration with as low a
Signature of the Student
Signature of Supervisor
Date:
Date:
III
ACKNOWLEDGEMENTS
Firstly, I would like to express my sincere gratitude to Dr. R.N. Sahah, Director BPD who has given me an opportunity to understand and apply engineering concepts in real life problems through the Project.
I am very grateful to Prof. Dr.A.M. Surendra Kumar, Project in-charge, for assisting me enthusiastically in the entire project. It is only with his guidance that the objectives of the project have been accomplished.
I V
TABLE OF CONTENTS
TITLE
PAGE NO
On
UNSTEADINESS IN AIRCRAFT DESIGN
By
AVIRAL TALWAR
2011A4PS152U
At
BITS Pilani Dubai Campus
Dubai International Academic City, Dubai
U.A.E
Second Semester, 2013-2014
A Report
On
UNSTEADINESS IN AIRCRAFT DESIGN
BY
AVIRAL TALWAR
2011A4PS152U
Prepared in Partial Fulfillment of the
Project Course: ME F366 Laboratory Project
At
BITS Pilani Dubai Campus
Dubai International Academic City, Dubai
UAE
Second Semester, 2013-2014
II
MECH
BITS Pilani, Dubai Campus
Dubai International Academic City, Dubai
UAE
Course name: Laboratory Project
Course number: ME F366
Duration: 23.02.2014 to 22.05.2014
Date of start: 23.02.2013
Date of submission: 22.05.2014
Title of Report: Unsteadiness in aircraft design
Name / ID Number: Aviral Talwar/ 2011A4PS152U
Discipline of Student: B.E (Hons) Mechanical Engineering
Name of Project Supervisor: Dr. A.M. Surendra kumar
Project Area: Aerodynamics, Fluid Dynamics, Elasticity
Abstract:
The traditional process of aerodynamic design is carried out manually by trial-and-error method. This process requires a large number of design engineers working alongside a huge budget. In order to overcome this manual method, the technologically driven software design using CFD will provide a cost effective optimal design method.
Software products for automatic aerodynamic design are intended to solve the basic problem of preliminary aerodynamic design: to develop a configuration with as low a
Signature of the Student
Signature of Supervisor
Date:
Date:
III
ACKNOWLEDGEMENTS
Firstly, I would like to express my sincere gratitude to Dr. R.N. Sahah, Director BPD who has given me an opportunity to understand and apply engineering concepts in real life problems through the Project.
I am very grateful to Prof. Dr.A.M. Surendra Kumar, Project in-charge, for assisting me enthusiastically in the entire project. It is only with his guidance that the objectives of the project have been accomplished.
I V
TABLE OF CONTENTS
TITLE
PAGE NO
References: [2] A. Betz, Verhalten von Wirbelsystemen, Z. Ang. Math. Mech. 12 (1932) 164–174. [9] Kalviste J. Aircraft stability characteristics at high angles of attack. AGARD-CP-235, Paper #29, 1978. Optimization,” NASA TM 86317, Oct. 1984. Application `a l’´ Etude des Effets des Retards,” La Recherche A´erospatiale, Vol. 2, 1995, pp Aircraft, Vol. 37, No. 5, 2000, pp. 833–839. Dynamics, Vol. 25, No. 5, 2002, pp. 985–987. 1 4% match (Internet from 04-Nov-2012)