Kryvokhatko I. Aerodynamic characteristics determination method for tandem-scheme aircraft

Українська версія

Thesis for the degree of Candidate of Sciences (CSc)

State registration number

0415U004616

Thesis Registration Form

0415U004616.pdf

Applicant for

Specialization

  • 05.07.01 - Аеродинаміка та газодинаміка літальних апаратів

01-10-2015

Specialized Academic Board

Д 26.062.05

Essay

The work is dedicated to developing of the aircraft longitudinal and lateral static aerodynamic characteristics determination method based on analytic, CFD and wind tunnel research. Aerodynamic characteristics of UAV with telescopic wing/wings research was performed. Airfoil choosing algorithm was developed taking into account both tandem-scheme and micro-UAV specificity (low Reynolds number). Tandem-scheme vortex system similarity criterions were defined. Wind tunnel test of non-rigid model with geometric variables (stagger, dihedral angle, wingspans) was performed.

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Files

Автореф_Кривохатько.doc

ДИССЕРТАЦИЯ_КРИВОХАТЬКО.doc

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