NUMERICAL ANALYSIS OF THE IMPACT OF SIDESLIP ANGLE ON LOAD OF THE GYROCOPTER STABILIZERS-Reference-Cited by-同舟云学术

NUMERICAL ANALYSIS OF THE IMPACT OF SIDESLIP ANGLE ON LOAD OF THE GYROCOPTER STABILIZERS

Published:2020-02-17 Issue:4 Volume:23 Page:114-122
ISSN:1648-7788
Container-title:Aviation
language:
Short-container-title:

Author:

Czyż Zbigniew¹^ORCID,Karpiński Paweł²

Affiliation:

1. Aeronautics Faculty, Polish Air Force University, 35 Dywizjonu 303 St., 08-521 Dęblin, Poland

2. Department of Thermodynamics, Fluid Mechanics and Aviation Propulsion Systems, Faculty of Mechanical Engineering, Lublin University of Technology, 36 Nadbystrzycka St., 20-618 Lublin, Poland

Abstract

The paper presents some of the works related to the project of modern gyrocopter construction with the possibility of a short start, known as "jump-start". It also presents a methodology related to numerical calculations using Computational Fluid Dynamics based on ANSYS Fluent three-dimensional solver. The purpose of the work was to calculate the forces and aerodynamic moments acting on the gyrocopter stabilizers. The calculations were carried out for a range of angle of attack α from –20° to +25° and for a sideslip angle β from 0° to 20°. Based on the calculations carried out, analysis of the impact of the slip angle on the load on the stabilizers has been made.

Publisher

Vilnius Gediminas Technical University

Subject

Aerospace Engineering

Reference25 articles.

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5. Aircraft directional stability prediction method by CFD

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