1. Bachelor Graduation Thesis on:
« Choice of parameters and design of units of a
supersonic passenger aircraft»
Student of 140 group:
R. D. Noutai
Professor:
I.V. Riabkov
Kharkov 2012

2. Conceptual Design Requirements:
Number of Passenger– 140
Flight Range– 6000 km
Cruise Speed – 900 Km/h
– 2200 км/ч Supersonic
Cruise Altitude– 16,4 Km
Maximum Speed – 2800 Km/h

3. Construction
Part

4. Самолеты прототипыIl-86
Tu-144
Concorde
Boeing 707
A 300

7. Aerodynamic Characteristics and Wing Structures

10. -100.00
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50.00
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0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 0.95 1
qb
qkr
q
Diagrams qy
в qy
кр
Diagrams Qy

11. Diagrams Mx Diagrams Mz

12. Construction of wing’s spar

14. Design of the engine mounting systems

16. Technology
Section
Development of the aircraft parts manufacturing technology
Sheet stamping and stamp design

18. Financial
Section

19. Cost of the airplane With engines and without engines
• The Ariplane will cost $57.211731 millions without
engines
• The Ariplane will cost $79.735885 millions with engines

20. Safety Section

21. Development of the air conditioning system

22. Special Section

23. Estimation of the gas emissions from turbines engines

24. Conclusion
Given the actual development of avation technology, we can
state our project will demonstrate human Intelligence and Art, proof of
our level of knowledge and excellence.
This is because the project depend on the equation of airplanes
existence, which not only add the masses of each component together
but also take in count their different property.

25. Thank you
for your attention