Taranenko I. The method of analysis thermal stressed state of skin panel stringers made of composites

Українська версія

Thesis for the degree of Candidate of Sciences (CSc)

State registration number

0411U000357

Thesis Registration Form

0411U000357.pdf

Applicant for

Specialization

  • 05.07.02 - Проектування, виробництво та випробування літальних апаратів

27-01-2011

Specialized Academic Board

Д 64.062.04

National Aerospace University "Kharkiv Aviation Institute"

Essay

The object of research - thin-walled load-carrying elements of aircraft (stringers, wing spars, beams, skin panels, fuselage panel etc.) made of composites; methods - general theory of elasticity of thin-walled structures, methods of analysis of physical-mechanical characteristics of anisotropic composites; dependencies for calculation linear and angle displacements of contour points of rods, practical recommendations considering physical-mechanical properties and geometry of cross-section, which have to be used at the stage of preliminary design of composite article; field of application - aviation and rocket building

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.