JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY HYDERABAD

AE703PC: FLIGHT VEHICLE DESIGN AND INSTRUMENTATION LAB

B.Tech IV Year I Semester (R16)

List of Experiments

  • 1. Specification of design requirements- mission profile-conceptual sketches, initial sizing.
  • 2. Airfoil and geometry selection, determination of thrust to weight ratio, wing loading.
  • 3. First sizing & configuration layout, crew station, passengers & payload.
  • 4. Baseline design- stability & control, performance and constraint analysis.
  • 5. Cost estimation, parametric analysis, optimization, refined sizing & trade studies.
  • 6. Determination of final baseline design configuration, preparation of specification report.
  • 7. Hydraulic system.
  • 8. Pneumatic system.
  • 9. Demonstration on (a) Landing gears (b) Shock absorbers (c) Electro-mechanical operations of Elevators, Rudder, Flap etc on an actual aircraft (d) Artificial Horizon, Airspeed Indicator,
  • 10. Instrument landing system.

REFERENCES:

  • 1. Jenkinson, L.R. and Marchman III, J. F., Aircraft Design Projects for Engineering Students,
  • 2. Butterworth Heinemann, 2003, ISBN: 0 7506 5772 3.
  • 3. Raymer, D.P., Aircraft Design: A Conceptual Approach, 3rd edn., AIAA Education Series, AIAA, 1999, ISBN: 1-56347-281-0.
  • 4. Fielding, J.P., Introduction to Aircraft Design, Cambridge University Press, 2005, ISBN: 0- 521-657222-9.AIAA Aerospace Design Engineer’s Guide, 5th edn., AIAA Education Series, 2003, ISBN 1-56347-590-1.
  • 5. Keane, A.J. And Nair, P.B., Computational Approaches for Aerospace Design, Wiley, 2005, ISBN:0-470-85540-1.
  • 6. Taylor, J., Jane’s All the World Aircraft, latest edition, Jane’s, London.
  • 7. Stinton, The Design of the Airplane, second edition, AIAA, 2001, ISBN: 0-56347- 524-6. R16 B.TECH AERONAUTICAL ENGG.

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