Kondratiev A. Optimum designing of composite airframes with honeycomb filler on a basis of finite-element method and analytic models synthesis.

Українська версія

Thesis for the degree of Candidate of Sciences (CSc)

State registration number

0409U002020

Thesis Registration Form

0409U002020.pdf

Applicant for

Specialization

  • 05.07.02 - Проектування, виробництво та випробування літальних апаратів

20-03-2009

Specialized Academic Board

Д 64.062.04

National Aerospace University "Kharkiv Aviation Institute"

Essay

Object – projecting and designing of products for aerospace purpose. Goal – flying vehicles’ frame mass decrease by means of their parameters optimization. Novelty – for the first time developed conception of composite frames’ mass minimization, models of improvement of honeycomb filler PMC, local zones classifier and approach to reinforcement parameters optimization on mass. Results – rocket-carrier «Cyclone-4» head fairing mass effectiveness raise, improved honeycomb filler PMC. Industry – airplane and rocket production.

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Files

Автореферат.doc

Диссертация.doc

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