Aircraft Design and Testing detail syllabus for Aeronautical Engineering (Aero), 2019-20 scheme is taken from AKTU official website and presented for AKTU students. The course code (RAE087), 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 8th sem syllabus for b.tech 2019-20 scheme aktu you can visit Aero 8th Sem syllabus for B.Tech 2019-20 Scheme AKTU Subjects. For all other Departmental Elective-6 subjects do refer to Departmental Elective-6. The detail syllabus for aircraft design and testing is as follows.
Unit I
For the complete syllabus, results, class timetable and more kindly download iStudy. It’s a lightweight, easy to use, no images, no pdfs platform to make student’s life easier.
Unit II
Design Considerations: Wing. Wing Design: Air foil. Wing Design: t/c, Camber and Leading-Edge Radius.
Wing Design: Aspect Ratio. Wing Design: Sweep, Twist and Taper Ratio. Wing Arrangements.Tail Arrangements.Aircraft Structure.Wing Loading and Power Loading.Thrust Loading and Wing Loading.Thrust Loading. Wing Loading.Wing Loading: Manoeuvre, Climb and glide. Take-off: Wing Loading and Thrust Loading. Take-off and landing distance. Stall and High Life Devices.
Unit III
Wing Loading: Take-off and Landing.Revision (Wing Loading and Thrust Loading).Numerical: Wing Loading. Wing Loading: Designers Approach.Wing Loading: Designers Approach. Stability Considerations.Static Stability Basics.Wing and tail contribution to Longitudinal Static Stability.Conceptual Design.Conceptual design Elevator Effectiveness.Elevator Effectiveness.Numerical – pitching moment. Numerical – Elevator Effectiveness.Aircraft Maintenance Guidelines.Inspection for Aircraft.Numerical of Weight Fraction
Unit IV
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Unit V
Measuring devices in Test Section: Pitot tube static tube, yaw probes, five-hole probe, hot wire anemo-meters. Flow visualization techniques oil flow and smock flow. Flow field pressure measurements, Schlieren, shadowgraph and interferometer technique, laser Doppler, hot wire PIV technique, Wind tunnel balances, mechanical and strain gauge balances and their design. Scale effects. Non – aeronautical use of wind tunnels.
Books and References:
- Daniel P Raymer, Aircraft Design: A conceptual approach, AIAA Series, 1992.
- D Stanton, The Design of Airplane, GRANADA, UK 1983.
- John D Anderson (Jr.), Airplane Performance and Design, McGraw Hill 1999.
- E Torenbeek, Synthesis of Airplane Design.
For detail syllabus of all other subjects of B.Tech Aero, 2019-20 regulation do visit Aero 8th Sem syllabus for 2019-20 Regulation.
Don’t forget to download iStudy for the latest syllabus, results, class timetable and more.