Kireyev I. The technology of winding composite wings of small lengthening of unmanned aerial vehicles

Українська версія

Thesis for the degree of Candidate of Sciences (CSc)

State registration number

0411U005095

Thesis Registration Form

0411U005095.pdf

Applicant for

Specialization

  • 05.07.02 - Проектування, виробництво та випробування літальних апаратів

17-06-2011

Specialized Academic Board

Д64.062.04

Essay

Object - keystone wing small extension of the CM; Purpose - to reduce the mass of small trapezoidal wing extension due to higher degree of properties of composite materials, development through technology solutions built on the method of continuous winding; research methods - methods of differential geometry and analysis, apparatus mathematical analysis, theory of differential equations for the pro-management and mathematical modeling of computer models used system's- computer mathematics- a model of continuous winding wing skin small extension of the composites based on tow and tapes; first solved the problem of definition design and technological parameters of winding and installed a management program for architecture, winding machine CNC

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Files

aref.pdf

dis.doc

dis.pdf

акт 1.doc

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