Kolomiytsev A. The Method of accounting and experimental shape determination of the special purpose projectile with given aerodynamic properties.

Українська версія

Thesis for the degree of Candidate of Sciences (CSc)

State registration number

0405U002987

Thesis Registration Form

0405U002987.pdf

Applicant for

Specialization

  • 05.07.01 - Аеродинаміка та газодинаміка літальних апаратів

10-06-2005

Specialized Academic Board

Д64.062.02

Essay

The object is aircraft (the projectile) with concave ogival nose and internal cavity; the purpose is development of the complex method of the designing free form projectile of the different purpose; the method is numerical simulation; the novelty is offered technology of the designing projectile, founded on aerodynamic approach and presentations; the result is designed projectile, which form provides the given conditions of the diffusing to kinetic energy on trajectory; it is recommended for use in institutions, concerning with questions of the designing ammunition and their of criminal researches.

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Files

Автореферат диссертации Коломийцева А.В..doc

Диссертация Коломийцева А.В..doc

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