Buchumschlag

Dynamic instability of rockets deflectors in flight

The parabolic shells are widely used in rockets production and aircrafts construction. These shells are streamed by gas flow. The interaction of the thin-walled structures with gas stream can lead to the self-sustained vibrations with large amplitudes. As follows from the above-presented survey, the...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Datum:	2014
Hauptverfasser:	Чернобрывко, М. В., Аврамов, К. В., Романенко, В. Н., Батутина, Т. Я., Пирог, В. А.
Format:	Artikel
Sprache:	Russisch
Veröffentlicht:	Інститут енергетичних машин і систем ім. А. М. Підгорного Національної академії наук України 2014
Schlagworte:	parabolic shell rockets deflectors assumed-modes method Mach number supersonic gas stream УДК 539.3
Online Zugang:	https://journals.uran.ua/jme/article/view/27186
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!
Назва журналу:	Energy Technologies & Resource Saving

Institution

Energy Technologies & Resource Saving

Ähnliche Einträge

Dynamic instability of rockets deflectors in flight
von: Чернобрывко, М. В., et al.
Veröffentlicht: (2014)

Dynamic instability of rockets deflectors in flight
von: M. V. Chernobryvko, et al.
Veröffentlicht: (2014)

LARGE-SCALE DISTURBANCES IN THE TERRESTRIAL IONOSPHERE, WHICH ACCOMPANIED THE LAUNCHES AND FLIGHTS OF POWERFUL ROCKETS
von: Chernogor, L. F.
Veröffentlicht: (2025)

AN ANTHOLOGY OF THE DISTINGUISHED ACHIEVEMENTS IN SCIENCE AND TECHNIQUE. PART 51: ROCKET-SPACE TECHNOLOGY DESIGNER SERGEY KOROLEV AND HIS ACCOMPLISHMENTS IN MISSILE DESIGN
von: Baranov, M. I.
Veröffentlicht: (2019)

AN ANTHOLOGY OF THE DISTINGUISHED ACHIEVEMENTS IN SCIENCE AND TECHNIQUE. PART 52: ROCKET-SPACE TECHNOLOGY DESIGNER MIKHAIL YANGEL AND HIS ACCOMPLISHMENTS IN MISSILE DESIGN
von: Baranov, M. I.
Veröffentlicht: (2019)

Optimization of flights of the spacecrafts with electro-rocket engines
von: Ja. V. Tkachenko
Veröffentlicht: (2014)

Semi-analytical finite element method for deflected mode of ribbed cylindrical shells
von: Аврамов, К. В., et al.
Veröffentlicht: (2014)

Semi-analytical finite element method for deflected mode of ribbed cylindrical shells
von: Аврамов, К. В., et al.
Veröffentlicht: (2014)

An anthology of outstanding achievements in science and technology. Part 18: Rocket engineering and near-space exploration.
von: Baranov, M. I.
Veröffentlicht: (2014)

Determination of model parameters of rocket stabilization system in flight
von: V. V. Avdeev
Veröffentlicht: (2021)

NUMERICAL CALCULATION OF PARABOLIC AND PARABOLIC THROUGH CONCENTRATOR PARAMETERS FOR THE SOLAR POWER SYSTEM BASED ON STIRLING ENGINE
von: Stoudenets, V., et al.
Veröffentlicht: (2019)

AN ANTHOLOGY OF THE DISTINGUISHED ACHIEVEMENTS IN SCIENCE AND TECHNIQUE. PART 50: ROCKET-SPACE TECHNOLOGY DESIGNER WERNHER VON BRAUN AND HIS ACCOMPLISHMENTS IN MISSILE DESIGN
von: Baranov, M. I.
Veröffentlicht: (2019)

Travelling wave deflector for free electron laser
von: Anisimov, A.A., et al.
Veröffentlicht: (2010)

Comparative analysis of the efficiency of constant power throttled rocket engines for interorbital flights to geostationar
von: Ju. Vasilev, et al.
Veröffentlicht: (2021)

Periodic, almost periodic and chaotic forced oscillations of the sloping cantilever shell under geometrically nonlinear deformation
von: Малышев, С. Е., et al.
Veröffentlicht: (2017)

Periodic, almost periodic and chaotic forced oscillations of the sloping cantilever shell under geometrically nonlinear deformation
von: Малышев, С. Е., et al.
Veröffentlicht: (2017)

Interaction of shallow shell with subcritical potential stream
von: Аврамов, К. В.
Veröffentlicht: (2015)

Interaction of shallow shell with subcritical potential stream
von: Аврамов, К. В.
Veröffentlicht: (2015)

On the adaptation of bifunctional systems of liquid-propellant rocket thrust vec-tor control to modern methods and systems of space rocket stage flight control
von: T. A. Kovalenko, et al.
Veröffentlicht: (2017)

ANALYSIS OF SOLAR RADIATION CONCENTRATION PLANTS TO ENSURE THE OPERATION OF THE STIRLING ENGINE
von: Golovko, V., et al.
Veröffentlicht: (2023)

Analysis of nonlinear forces acting on rotor shaft in journal bearings
von: Борисюк, А. В., et al.
Veröffentlicht: (2016)

Analysis of nonlinear forces acting on rotor shaft in journal bearings
von: Борисюк, А. В., et al.
Veröffentlicht: (2016)

Effect of parameters of journal bearings on selfvibration of one-disk rotor
von: Аврамов, К. В., et al.
Veröffentlicht: (2016)

Effect of parameters of journal bearings on selfvibration of one-disk rotor
von: Аврамов, К. В., et al.
Veröffentlicht: (2016)

Динамическая устойчивость параболических оболочек в сверхзвуковом потоке
von: Аврамов, К.В., et al.
Veröffentlicht: (2014)

Динамическая неустойчивость обтекателей ракет-носителей в полете
von: Чернобрывко, М.В., et al.
Veröffentlicht: (2014)

Comparative Analysis of Ionospheric Effects During “Proton” Rocket Flights under Different States of Space Weather
von: Chernogor, L. F., et al.
Veröffentlicht: (2012)

Determination of initial characteristics of fuel components droplet cloud derived from in-flight explosion of carrier rocket
von: O. V. Pilipenko, et al.
Veröffentlicht: (2017)

Узагальнені крайові значення розв'язків півлінійних еліптичних та параболічних рівнянь
von: Лопушанська, Г.П., et al.
Veröffentlicht: (2007)

OPTICAL SENSOR FOR SURFACE PROFILE MONITORING OF PARABOLIC ANTENNA FOR MILLIMETER AND SUBMILLIMETER ASTRONOMY
von: Chechetkin, D. L., et al.
Veröffentlicht: (2016)

Recursive method for constructing linear convolution algorithms of various lengths using hypercomplex number systems.
von: Kalinovsky, Ya. A., et al.
Veröffentlicht: (2019)

Non-stationary vibration of electroelastic shallow spherical shell
von: Янчевський, І. В.
Veröffentlicht: (2015)

Non-stationary vibration of electroelastic shallow spherical shell
von: Янчевський, І. В.
Veröffentlicht: (2015)

Parametric synthesis of the digital stabilizer of the space stage of the rocket-carrier with a liquid reactive engine at the active section of the flight trajectory
von: E. E. Aleksandrov, et al.
Veröffentlicht: (2020)

Structure of an algoritsm for quick two-dimensional convolution by means of isomorphing hypercomplex numerical systems
von: Kalinovsky, Ya. A., et al.
Veröffentlicht: (2018)

Dynamic Processes During the Through-plastic-damper Shock Interaction of Rocket Fairing Separation System Components
von: Zaytsev, Boris F., et al.
Veröffentlicht: (2018)

Dynamic Processes During the Through-plastic-damper Shock Interaction of Rocket Fairing Separation System Components
von: Zaytsev, Boris F., et al.
Veröffentlicht: (2018)

Numerical Analysis of Working Processes in the Blade Channels of the Highly-Loaded Turbine of a Marine Gas Turbine Engine, Using a Refined Finite Element Model
von: Morhun, Serhii O.
Veröffentlicht: (2019)

Numerical Analysis of Working Processes in the Blade Channels of the Highly-Loaded Turbine of a Marine Gas Turbine Engine, Using a Refined Finite Element Model
von: Morhun, Serhii O.
Veröffentlicht: (2019)

Strength of Composite Transport and Launch Container for Rocket Launch
von: Аврамов, К. В., et al.
Veröffentlicht: (2024)