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
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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
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
ConstructionPart
Самолеты прототипыIl-86
Tu-144
Concorde
Boeing 707
A 300
Aerodynamic Characteristics and Wing Structures
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Diagrams Qy
Diagrams Mx Diagrams Mz
Construction of wing’s spar
Design of the engine mounting systems
Technology Section
Development of the aircraft parts manufacturing technology Sheet stamping and stamp design
FinancialSection
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
Safety Section
Development of the air conditioning system
Special Section
Estimation of the gas emissions from turbines engines
ConclusionGiven 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.
Thank you for your attention
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