COMPUTATIONAL MODELING OF AERODYNAMIC INTERFERENCE OF HELICOPTER MAIN AND TAIL ROTORS AT THE SPECIAL FLIGHT REGIMES

This article is concentrated on modeling and researching of aerodynamic characteristics of main and tail rotors’ combination of a single-rotor helicopter scheme. Non-linear free wake vortical model with diffusion of free wake is used. The model is constructed on the base of Helicopter Design Faculty...

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Published in:Научный вестник МГТУ ГА
Main Authors: Y. M. Ignatkin, P. V. Makeev, A. I. Shomov
Format: Article
Language:Russian
Published: Moscow State Technical University of Civil Aviation 2016-11-01
Subjects:
Online Access:https://avia.mstuca.ru/jour/article/view/9
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author Y. M. Ignatkin
P. V. Makeev
A. I. Shomov
author_facet Y. M. Ignatkin
P. V. Makeev
A. I. Shomov
author_sort Y. M. Ignatkin
collection DOAJ
container_title Научный вестник МГТУ ГА
description This article is concentrated on modeling and researching of aerodynamic characteristics of main and tail rotors’ combination of a single-rotor helicopter scheme. Non-linear free wake vortical model with diffusion of free wake is used. The model is constructed on the base of Helicopter Design Faculty, MAI. There was analyzed a number of special flight regimes of a helicopter. There were counted aerodynamic characteristics of rotors.
format Article
id doaj-art-d14d59752ece4c19aa2b584927c628b9
institution Directory of Open Access Journals
issn 2079-0619
2542-0119
language Russian
publishDate 2016-11-01
publisher Moscow State Technical University of Civil Aviation
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spelling doaj-art-d14d59752ece4c19aa2b584927c628b92025-08-20T03:43:21ZrusMoscow State Technical University of Civil AviationНаучный вестник МГТУ ГА2079-06192542-01192016-11-01020047549COMPUTATIONAL MODELING OF AERODYNAMIC INTERFERENCE OF HELICOPTER MAIN AND TAIL ROTORS AT THE SPECIAL FLIGHT REGIMESY. M. Ignatkin0P. V. Makeev1A. I. Shomov2МАИМАИМАИThis article is concentrated on modeling and researching of aerodynamic characteristics of main and tail rotors’ combination of a single-rotor helicopter scheme. Non-linear free wake vortical model with diffusion of free wake is used. The model is constructed on the base of Helicopter Design Faculty, MAI. There was analyzed a number of special flight regimes of a helicopter. There were counted aerodynamic characteristics of rotors.https://avia.mstuca.ru/jour/article/view/9computational modelinginterferencemain rotortail rotorspecial flight regimes
spellingShingle Y. M. Ignatkin
P. V. Makeev
A. I. Shomov
COMPUTATIONAL MODELING OF AERODYNAMIC INTERFERENCE OF HELICOPTER MAIN AND TAIL ROTORS AT THE SPECIAL FLIGHT REGIMES
computational modeling
interference
main rotor
tail rotor
special flight regimes
title COMPUTATIONAL MODELING OF AERODYNAMIC INTERFERENCE OF HELICOPTER MAIN AND TAIL ROTORS AT THE SPECIAL FLIGHT REGIMES
title_full COMPUTATIONAL MODELING OF AERODYNAMIC INTERFERENCE OF HELICOPTER MAIN AND TAIL ROTORS AT THE SPECIAL FLIGHT REGIMES
title_fullStr COMPUTATIONAL MODELING OF AERODYNAMIC INTERFERENCE OF HELICOPTER MAIN AND TAIL ROTORS AT THE SPECIAL FLIGHT REGIMES
title_full_unstemmed COMPUTATIONAL MODELING OF AERODYNAMIC INTERFERENCE OF HELICOPTER MAIN AND TAIL ROTORS AT THE SPECIAL FLIGHT REGIMES
title_short COMPUTATIONAL MODELING OF AERODYNAMIC INTERFERENCE OF HELICOPTER MAIN AND TAIL ROTORS AT THE SPECIAL FLIGHT REGIMES
title_sort computational modeling of aerodynamic interference of helicopter main and tail rotors at the special flight regimes
topic computational modeling
interference
main rotor
tail rotor
special flight regimes
url https://avia.mstuca.ru/jour/article/view/9
work_keys_str_mv AT ymignatkin computationalmodelingofaerodynamicinterferenceofhelicoptermainandtailrotorsatthespecialflightregimes
AT pvmakeev computationalmodelingofaerodynamicinterferenceofhelicoptermainandtailrotorsatthespecialflightregimes
AT aishomov computationalmodelingofaerodynamicinterferenceofhelicoptermainandtailrotorsatthespecialflightregimes