Gagauz P. Rational design of composite skin panels for aircrafts

Українська версія

Thesis for the degree of Candidate of Sciences (CSc)

State registration number

0411U000359

Thesis Registration Form

0411U000359.pdf

Applicant for

Specialization

  • 05.07.02 - Проектування, виробництво та випробування літальних апаратів

28-01-2011

Specialized Academic Board

Д 64.062.04

National Aerospace University "Kharkiv Aviation Institute"

Essay

Object is aircraft skin panels made of composite materials; the aim is to reduce weight of composite panels by lay-up optimization; the methods are classical mechanics of laminated materials, differential calculus and calculus of variations; the novelty lie in analytical solutions of laminate optimization problem with strength, buckling and stiffness constraints; results - definition of typical omptimal lay-up configurations; the field is airplane and rocket production

Read more

Files

aref.doc

dis.doc

Similar theses

0521U101549

Kapitanova Liudmyla Valeriivna

Analysis and Synthesis of Takeoff and Landing Performance of Transport Category Airplanes

0421U102094

Degtiarov Maksym Olexandrovych

Selection of rational parameters and reduction of material consumption of tail compartments of launch vehicles

0421U101554

Mishchenko Olexandra Vasylivna

Methodological support for the design of electrodynamic space tethered systems

0421U101553

Syutkina-Doronina Svetlana Vasylivna

A methodology for the optimization of design characteristics of single-stage guided rockets with solid rocket motors

0421U101555

Siedykh Ihor Viktorovych

The choice of design parameters of inertial means of ensuring the continuity of propellant in the tanks of the space stages of launch vehicles.