Helicopter Theory Aero 7th Sem Syllabus for BE 2017 Regulation Anna Univ (Professional Elective II) detail syllabus for Aeronautical Engineering (Aero), 2017 regulation is collected from the Anna Univ official website and presented for students of Anna University. The details of the course are: course code (AE8004), Category (PE), Contact Periods/week (3), Teaching hours/week (3), Practical Hours/week (0). The total course credits are given in combined syllabus.
For all other aero 7th sem syllabus for be 2017 regulation anna univ you can visit Aero 7th Sem syllabus for BE 2017 regulation Anna Univ Subjects. For all other Professional Elective II subjects do refer to Professional Elective II. The detail syllabus for helicopter theory is as follows.
Course Objective:
- To make the student familiarize with the principles involved in helicopters and to study the performance and stability aspects of Helicopter under different operating conditions.
Unit I
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Unit II
Aerodynamics of Rotor Blade
Aerofoil characteristics in forward flight, Hovering and Vortex ring state, Blade stall, maximum lift of the helicopter calculation of Induced Power, High speed limitations; parasite drag, power loading, ground effect.
Unit III
Power Plants and Flight Performance
Piston engines, Gas turbines, Ramjet principle, Comparative performance, Horsepower required, Range and Endurance, Rate of Climb, Best Climbing speed, Ceiling in vertical climb, Autorotation.
Unit IV
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Unit V
Rotor Vibrations
Dynamic model of the rotor, Motion of the rigid blades, flapping motion, lagging motion, feathering motion, Properties of vibrating system, phenomenon of vibration, fuselage response, vibration absorbers, Measurement of vibration in flight. Rotor Blade Design: General considerations, Airfoil selection, Blade construction, Materials, Factors affecting weight and cost, Design conditions, Stress analysis.
Course Outcome:
- To perform the Aerodynamics calculation of Rotor blade
- To perform stability and control characteristics of Helicopter
- To perform and control Rotor vibration
- Apply Momentum and simple blade element theories to helicopters rotor blades.
- Analyze the power requirements in forward flight and associated stability problems of helicopter.
Text Books:
- John Fay, “The Helicopter and How It Flies”, Himalayan Books 1995
- Lalit Gupta, “Helicopter Engineering”, Himalayan Books New Delhi 1996
References:
- Joseph Schafer, “Basic Helicopter Maintenance”, Jeppesen 1980
- R W Prouty, Helicopter Aerodynamics, Phillips Pub Co, 1993.
For detail syllabus of all other subjects of BE Aero, 2017 regulation do visit Aero 7th Sem syllabus for 2017 Regulation.
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