AEROELASTIC STABILITY RESEARCH OF A CROSS-SHAPED FLYING VEHICLE

Aleksandr Grigorievich Narizhny; Vsevolod Igorevich Smyslov; Stanislav Igorevich  Sychev

doi:10.1615/TsAGISciJ.2014011150

TsAGI Science Journal

Главный редактор: Sergei Leonidovich Chernyshev (open in a new tab)

Ассоциированный редактор: Ivan Vladimirovich Egorov (open in a new tab)

International Executive Editorial Advisors: M. de Gliniasty (open in a new tab) C.W. Kauffman (open in a new tab) Jurgen Quest (open in a new tab) Gu Songfen (open in a new tab) Shinji Suzuki (open in a new tab)

Выходит 6 номеров в год

ISSN Печать: 1948-2590

ISSN Онлайн: 1948-2604

AEROELASTIC STABILITY RESEARCH OF A CROSS-SHAPED FLYING VEHICLE

Том 44, Выпуск 6, 2013, pp. 885-909

DOI: 10.1615/TsAGISciJ.2014011150

Get access

Aleksandr Grigorievich Narizhny
Central Aerohydrodynamic Institute (TsAGI), 1 Zhukovsky Str., Zhukovsky, Moscow Region, 140180, Russia

Vsevolod Igorevich Smyslov
Central Aerohydrodynamic Institute (TsAGI), Zhukovsky str. 1, Zhukovsky, 140180 Russia

Stanislav Igorevich Sychev
Tactical Missiles Corporation, 7 Ilicha Str., Korolev, Moscow Region, 141075, Russia

Краткое описание

Computational and experimental research to prevent self-oscillations inflight of an elastic maneuverable flying vehicle (FV) with an automatic control system (CS) is presented. The methods and means of FV ground modal (resonance) testing are presented. They are used to correct the FV dynamic model used in the calculation of flutter, to investigate experimentally the aeroelastic stability, to characterize experimentally the CS with electric drive in the frequency range of elastic oscillations, and to determine the elastic FV-CS stability margin. Some examples are presented.

Ключевые слова: aeroelastic stability, flutter, ground resonance testing, automatic control system (CS)

ЦИТИРОВАНО В

Bykov A. V., Parafes S. G., Smyslov V. I., RESEARCH FEATURES OF AEROELASTIC OSCILLATIONS OF UNMANNED AERIAL VEHICLES WITH ELECTRIC ACTUATOR OF RUDDERS, Civil Aviation High TECHNOLOGIES, 21, 4, 2018. Crossref
Berns V. A., Dolgopolov A. V., Zhukov E. P., Marinin D. A., Influence of the suspension system on the accuracy of the aircraft modal testing results, VESTNIK of Samara University. Aerospace and Mechanical Engineering, 15, 1, 2016. Crossref

535 Просмотры статей 11 Загрузка статей Метрики

535 ПРОСМОТРЫ 11 ЗАГРУЗКИ 2 Crossref ЦИТАТЫ Google
Scholar ЦИТАТЫ

Статьи с похожим содержанием:

Stabilization of the Modulation Characteristic of Generating Transducers Telecommunications and Radio Engineering, Vol.69, 2010, issue 3
V. A. Pimenov, O. N. Katkov, A. I. Eremenko

MATHEMATICAL MODELING OF MULTIFUNCTIONAL DEVICES FOR FREQUENCY MODULATION AND DEMODULATION OF HIGH-FREQUENCY SIGNALS Telecommunications and Radio Engineering, Vol.72, 2013, issue 12
I. A. Malyutina, A. A. Golovkov, V. A. Golovkov

DYNAMIC NEURAL NETWORK AS A MODEL OF VISCOELASTIC MEDIA Composites: Mechanics, Computations, Applications: An International Journal, Vol.9, 2018, issue 4
Yu. A. Basistov, Alexander N. Danilin, Yuri G. Yanovsky, Yulia N. Karnet

Atomic-fractal Functions in Problems of Antenna Synthesis Telecommunications and Radio Engineering, Vol.56, 2001, issue 6&7
Victor Filippovich Kravchenko, Vladimir Mikhailovich Masyuk, Aleksander Alekseevich Potapov

IDENTIFICATION OF MATHEMATICAL MODEL OF MULTILAYER THERMAL INSULATION ICHMT DIGITAL LIBRARY ONLINE, Vol.0, 2010, issue
Oleg M. Alifanov, Vivaldo M. Gonzalez, Aleksey V. Nenarokomov

Последний выпуск

KIRILL IVANOVICH SYPALO−50TH ANNIVERSARY NUMERICAL STUDY OF THE DISTURBANCES GENERATED BY MICROJETS IN A SUPERSONIC FLAT-PLATE BOUNDARY LAYER Andrei Valerievich Novikov, Alexander Vitalyevich Fedorov, Ivan Vladimirovich Egorov, Anton Olegovich Obraz, Nikolay Nikolaevich Semenov ANALYSIS OF THE MOVING DETONATION INTERACTION WITH TURBULENT BOUNDARY LAYERS IN A DUCT ON THE BASIS OF NUMERICAL SIMULATION Vladimir Anatolievich Sabelnikov, Vladimir Viktorovich Vlasenko, Sergey Sergeyevich Molev EXPERIMENTAL STUDY OF COUNTERFLOW BLOWING IN HIGH-SPEED FLOW THROUGH AN ASYMMETRIC SLOT IN THE LEADING EDGE OF A SHARP WEDGE Eduard Borisovich Vasilevskii, Ivan Valeryevich Ezhov, Pavel Vladimirovich Chuvakhov ASYMPTOTIC SOLUTIONS TO HYPERSONIC BOUNDARY LAYER EQUATIONS ON A FLAT WING WITH A POINT OF INFLECTION ON THE LEADING EDGE Georgiy Nikolaevich Dudin, Aleksey Vyacheslavovich Ledovskiy WAVE MODEL OF ORGANIZED STRUCTURES IN A TURBULENT BOUNDARY LAYER ON A PLATE WITH ZERO LONGITUDINAL PRESSURE GRADIENT Vladimir Alekseevich Zharov, Igor Ivanovich Lipatov, Rami Salah Saber Selim NUMERICAL SIMULATION OF THE FLOW AROUND LANDSCAPE FRAGMENTS AND SOLUTION VERIFICATION Viktor Viktorovich Vyshinsky, Koang T'in' Zoan POLYNOMIAL REPRESENTATION OF THERMODYNAMIC PROPERTIES OF COMBINED FUEL SYSTEMS IN RAMJET SIMULATION MODELS Timur Romanovich Zuev, Mikhail Semenovich Tararyshkin A MODEL TEST METHODOLOGY FOR THE INVESTIGATION OF AN ELASTICALLY SCALED MAIN ROTOR Maxim Andreyevich Ledyankin , Sergey Anatolyevich Mikhailov, Dmitry Valeryevich Nedel'ko, Timur Arturovich Agliullin INDEX, VOLUME 51, 2020