Abbas F. An experimental determination technique of vortex generators influence on wing aerodynamic characteristics on various angles of attack

Українська версія

Thesis for the degree of Candidate of Sciences (CSc)

State registration number

0408U005068

Thesis Registration Form

0408U005068.pdf

Applicant for

Specialization

  • 05.07.01 - Аеродинаміка та газодинаміка літальних апаратів

13-11-2008

Specialized Academic Board

Д 26.062.05

Essay

The thesis is devoted to the solution of an actual problem of improving the flow characteristics of a wing surface on operation angles of attack, optimization of aerodynamic characteristics of the airplane on large angles of attack, take-off and climb regimes.Experimental researches of a boundary layer control on a curvilinear surface of a wing section and the airplane have been executed in the thesis for estimating the vortex generators influence on integral aerodynamic characteristics.

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Files

аббас фадиль махмуд.doc

автореферат Аббас.doc SHK-автореферат Аббас.doc SHK.doc

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