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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

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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

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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