High Speed Aerodynamics (Dept Elec-III) (2180105)   Old Code : 180105

6
Credit
4 + 0 + 2
Lect + Tuto + Pract
Teaching Scheme
70 + 20 + 10
ESE + PA + ALA
Theory Marks
20 + 10 + 20
ESE + OEP + PA
Practical Marks
ESE - End Semester Examination, PA - Progress Assessment, ALA - Active Learning Assignments, OEP -Open Ended Problem


Prerequisite
Basics of Fluid Mechanics, Aerodynamics I, Computational Fluid Dynamics, Aerodynamics II, Boundary Layer Theory
Rationale
High Speed Aerodynamics is one of the core areas in the field of aviation. The concepts of High Speed Aerodynamics are vitally important to the aeronautical engineer
Course Outcome
After learning the course the students should be able to:
To know about the basic fundamentals of High Speed Aerodynamics, Wind tunnel, Understand basic terms used in Supersonic flow and Hypersonic flow, Understand the effect of the flow on the aircraft.

Active Learning
Preparation of power-point slides, which include videos, animations, pictures, graphics for better understanding theory and practical work – The faculty will allocate chapters/ parts of chapters to groups of students so that the entire syllabus to be covered. The power-point slides should be put up on the web-site of the College/ Institute, along with the names of the students of the group, the name of the faculty, Department and College on the first slide. The best three works should submit to GTU.