Aircraft Evaluation detail syllabus for Aeronautical Engineering (Aero), 2019-20 scheme is taken from AKTU official website and presented for AKTU students. The course code (RAE064), and for exam duration, Teaching Hr/Week, Practical Hr/Week, Total Marks, internal marks, theory marks, and credits do visit complete sem subjects post given below.
For all other aero 6th sem syllabus for b.tech 2019-20 scheme aktu you can visit Aero 6th Sem syllabus for B.Tech 2019-20 Scheme AKTU Subjects. For all other Departmental Elective-2 subjects do refer to Departmental Elective-2. The detail syllabus for aircraft evaluation is as follows.
Unit 1
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Unit 2
Aircraft Equipment: Cockpit layout and instrumentation, automatic landing system, Air Data Computer, ICAO Landing Categories, Communication and navigation equipment and their functions in general. Flight Recorder and Cockpit Voice Recorder and related regulatory requirements and there passenger amenities like passenger address system, crew intercom; music reproducer etc., Emergency facilities equipment and related regulation.Weather radar and its uses.Environmental control, air conditioning and pressurization their significance and necessity.
Unit 3
AircraftScheduling: Factor affecting airlines schedules, Commercial operation, Technical Metro logical, Airport Facilitation- run -way Strength and related requirements, Load Classification. Criteria for runaway and aircraft, Air Traffic Control and other number and other ground Communication /navigation facilities-their relationship and effect on related aircraft equipment Airport emergency Facilities – Firefighting, First Aid etc. Total take-of weight Balance diagram, calculation of c.g. and it’s variation due to variation pay load and consumables.
Unit 4
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Unit 5
Principles of Aerodynamic Testing: Brief history of the development of different types of Aerodynamic testing facilities, Drop tests, Rotating f tests. low speeds high sub- sonic speed transonic supersonic and hyper – sonic wind tunnels. Wind tunnel types according to fabrications. Description and principle of operation, types of mode tests possible areas of application and limitations of each of the facilities. Basic principles of flight testing and performance reduction.
Books and References:
- G. Corning , Supersonic and Subsonic Airplane Design, Boz No, 14 , College park , Maryland, 196,
- K.D Wood Aerospace Vehicle Design Vol, -I Aircraft design, Johnson Publishing Co.
- A. Lebedinski, Lecture notes on Aircraft Design Department of Aeronautical Engineering, Indian Institute of Science, Bangalore
- F.K. Teichman, Air plane Design Manual , Sir Issac Pitman & sons Ltd, 1950
- C.D. Perkins and R,E, Hage, Airplane Performance Stability and Control, John Wily and Sons inc, 1963
- D.O. Dommasch, S,S, Sherby& T,F, Connolly, Airplane Aerodynamics , Sir Issac Pitman & sons Ltd,1961
- I.H. Abott& A,F, Von Doenhoff, Theory of Wing Section, Dover Publication Inc, 1959,
For detail syllabus of all other subjects of B.Tech Aero, 2019-20 regulation do visit Aero 6th Sem syllabus for 2019-20 Regulation.
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