UB Paderborn / Katalog / Suche / in CDI

Sortiert nach

Einfacher Volltextzugriff von (fast) überall

Installieren Sie die LibKey Nomad-Browsererweiterung und erhalten Sie von vielen Webseiten einfachen Zugriff auf lizenzierte Volltexte oder Open Access Publikationen. Mehr erfahren...

Investigation Method of the Static Strength of Structurally-Anisotropic Composite Panels According to a Refined Theory

Mechanics of composite materials, 2023-07, Vol.59 (3), p.553-568

2023

Volltextzugriff (PDF)

Stress state analysis of laminated shells with piezoelectric layers based on the refined theory

Journal of physics. Conference series, 2021-05, Vol.1925 (1), p.12022

2021

Volltextzugriff (PDF)

The Basic Stress—Strain State of a Circular Plate of Variable Thickness Based on a Nonclassical Theory

Journal of machinery manufacture and reliability, 2019, Vol.48 (1), p.54-60

Firsanov, V. V.

2019

Volltextzugriff (PDF)

The Stressed State of the “Boundary Layer” Type in Cylindrical Shells Investigated according to a Nonclassical Theory

Journal of machinery manufacture and reliability, 2018-05, Vol.47 (3), p.241-248

Firsanov, V. V.

2018

Volltextzugriff (PDF)

The Stress State in the Boundary Region of a Conical Shell according to a Refined Theory

Journal of machinery manufacture and reliability, 2021, Vol.50 (1), p.51-57

2021

Volltextzugriff (PDF)

H2AX phosphorylation at the sites of DNA double-strand breaks in cultivated mammalian cells and tissues

Clinical epigenetics, 2011-08, Vol.2 (2), p.283-297

2011

Volltextzugriff (PDF)

The Stress State of Composite Cylindrical Shells Based on Refined Theory with Allowance for the Piezoelectric Effect

Journal of machinery manufacture and reliability, 2021-07, Vol.50 (4), p.312-318

2021

Volltextzugriff (PDF)

Analytical Review of Account Methods and Experimental Approaches to Stress-Strain State Investigation of Structurally-Anisotropic Aircraft Panels Made from Composite Materials

IOP conference series. Materials Science and Engineering, 2020-09, Vol.927 (1), p.12067

2020

Volltextzugriff (PDF)

Mathematical Models and Methods for Calculating the Stress-Strain State of Aircraft Panels from Composite Materials Taking into Account the Production Technology

Mechanics of solids, 2020-05, Vol.55 (3), p.403-412

2020

Volltextzugriff (PDF)

Study of stress-deformed state of rectangular plates based on nonclassical theory

Journal of machinery manufacture and reliability, 2016-11, Vol.45 (6), p.515-521

Firsanov, Val. V.

2016

Volltextzugriff (PDF)

MATHEMATICAL MODELS OF THE IMPROVEMENTED CALCULATION ON DURABILITY OF CONTINUOUS AVIATION CONNECTIONS WITH ACCOUNT OF THEIR COMPLIANCE

Stroitelʹnaâ mehanika inženernyh konstrukcij i sooruženij (Online), 2015-06 (3), p.58-69

V V Firsanov

2015

Volltextzugriff (PDF)

Determination of the Integral Content of the Components of Substances in the Control, Recording, and Monitoring of Production and Generation of Waste Products in Industrial Quantities

Measurement techniques, 2018-05, Vol.61 (2), p.182-191

2018

Volltextzugriff (PDF)

Stressed state "boundary layer" in a round plate of variable thickness according to refined theory

IOP conference series. Materials Science and Engineering, 2020-05, Vol.868 (1), p.12002

2020

Volltextzugriff (PDF)

BASE NEUTRAL SURFASE SELECTION FOR OPTIMAL DESIGN OF STRUCTURALLY-ANISOTROPIC AIRCRAFT PANELS MADE FROM COMPOSITE MATERIALS WITH REFINED BUCKLING THEORY RESTRICTIONS

PNRPU Mechanics Bulletin, 2023-12 (3), p.43-52

2023

Volltextzugriff (PDF)

Buckling Problem Statement and Approaches to Buckling Problem Investigation of Structurally-Anisotropic Aircraft Panels Made from Composite Materials

IOP conference series. Materials Science and Engineering, 2020-01, Vol.714 (1), p.12007

2020

Volltextzugriff (PDF)

BERNOULLI HYPOTHESES IN THE PROBLEM OF BENDING A MECHANICALLY INCOMPRESSIBLE BEAM

PNRPU Mechanics Bulletin, 2023-12 (4)

Firsanov, V. V

2023

Volltextzugriff (PDF)

THE LOCAL STRESS-STRAIN STATE OF A CYLINDRICAL SHELL ON THE BASIS OF THE THREE-DIMENSIONAL EQUATIONS OF THE THEORY OF ELASTICITY

Stroitelʹnaâ mehanika inženernyh konstrukcij i sooruženij (Online), 2013-06 (2), p.10-19

V V Firsanov

2013

Volltextzugriff (PDF)

Stress-Strain State and Buckling Problems of Structurally-Anisotropic Aircraft Panels Made of Composite Materials in View of Production Technology

Russian aeronautics, 2018-10, Vol.61 (4), p.524-532

2018

Volltextzugriff (PDF)

A method for estimating the certified value uncertainty of a multicomponent reference material

Reference materials, 2019-07, Vol.15 (1), p.5-13

2019

Volltextzugriff (PDF)

Gamma scintillation spectrometer calibration using the method of mathematical modeling

Radiatsionnaya Gygiena = Radiation Hygiene, 2020-12, Vol.13 (4), p.93-100

2020

Volltextzugriff (PDF)

Covariances in the variance of integral estimates of the contents of components of the substances’ composition in industrial quantities

Journal of physics. Conference series, 2022-03, Vol.2192 (1), p.12026

2022

Volltextzugriff (PDF)

INTERNAL IRRADIATION CONTROL AFTER RADIATION ACCIDENTS ON SHIPS AND VESSELS WITH NUCLEAR POWER UNITS: TASKS AND HARDWARE-METHODICAL SUPPORT

Radiacionnaâ gigiena, 2018-12, Vol.11 (4), p.64-70

2018

Volltextzugriff (PDF)

Elastoplastic stresses of a shell of revolution made from the material with linear hardening loaded by a force at the pole

Russian aeronautics, 2012-10, Vol.55 (4), p.366-372

2012

Volltextzugriff (PDF)

Analysis of edge effects and main stress-strain state of structurally-anisotropic aircraft panels comprising composite materials in refined theory

Composite Materials Constructions, 2021 (1), p.3-9

2021

Volltextzugriff (PDF)

ANALISIS OF THE “BOUNDARY LAYER“ STRESS-STRAIN STATE IN FRAMES OF THE NONCLASSICAL CYLINDRICAL SHELL THEORY

Stroitelʹnaâ mehanika inženernyh konstrukcij i sooruženij (Online), 2017-05 (3), p.71-76

Val V Firsanov

2017

Volltextzugriff (PDF)

1 – 25 von 76

Suche als RSS-Feed

Suchergebnisse filtern

Filter anzeigen

Nur zeigen

Geprüft (Peer-Review)
(64)
Mit Volltextzugriff
(42)

Publikationsform

Sprache

Englisch
(56)
Russisch
(24)

Erscheinungsjahr

n.n

Thema

15 weitere anzeigen...

Weniger anzeigen...

Neu hinzugefügt

... seit 7 Tagen
(1)

Menü

Weitere Dienste

Einstellungen

Investigation Method of the Static Strength of Structurally-Anisotropic Composite Panels According to a Refined Theory

Stress state analysis of laminated shells with piezoelectric layers based on the refined theory

The Basic Stress—Strain State of a Circular Plate of Variable Thickness Based on a Nonclassical Theory

The Stressed State of the “Boundary Layer” Type in Cylindrical Shells Investigated according to a Nonclassical Theory

The Stress State in the Boundary Region of a Conical Shell according to a Refined Theory

H2AX phosphorylation at the sites of DNA double-strand breaks in cultivated mammalian cells and tissues

The Stress State of Composite Cylindrical Shells Based on Refined Theory with Allowance for the Piezoelectric Effect

Analytical Review of Account Methods and Experimental Approaches to Stress-Strain State Investigation of Structurally-Anisotropic Aircraft Panels Made from Composite Materials

Mathematical Models and Methods for Calculating the Stress-Strain State of Aircraft Panels from Composite Materials Taking into Account the Production Technology

Study of stress-deformed state of rectangular plates based on nonclassical theory

MATHEMATICAL MODELS OF THE IMPROVEMENTED CALCULATION ON DURABILITY OF CONTINUOUS AVIATION CONNECTIONS WITH ACCOUNT OF THEIR COMPLIANCE

Determination of the Integral Content of the Components of Substances in the Control, Recording, and Monitoring of Production and Generation of Waste Products in Industrial Quantities

Stressed state "boundary layer" in a round plate of variable thickness according to refined theory

BASE NEUTRAL SURFASE SELECTION FOR OPTIMAL DESIGN OF STRUCTURALLY-ANISOTROPIC AIRCRAFT PANELS MADE FROM COMPOSITE MATERIALS WITH REFINED BUCKLING THEORY RESTRICTIONS

Buckling Problem Statement and Approaches to Buckling Problem Investigation of Structurally-Anisotropic Aircraft Panels Made from Composite Materials

BERNOULLI HYPOTHESES IN THE PROBLEM OF BENDING A MECHANICALLY INCOMPRESSIBLE BEAM

THE LOCAL STRESS-STRAIN STATE OF A CYLINDRICAL SHELL ON THE BASIS OF THE THREE-DIMENSIONAL EQUATIONS OF THE THEORY OF ELASTICITY

Stress-Strain State and Buckling Problems of Structurally-Anisotropic Aircraft Panels Made of Composite Materials in View of Production Technology

A method for estimating the certified value uncertainty of a multicomponent reference material

Gamma scintillation spectrometer calibration using the method of mathematical modeling

Covariances in the variance of integral estimates of the contents of components of the substances’ composition in industrial quantities

INTERNAL IRRADIATION CONTROL AFTER RADIATION ACCIDENTS ON SHIPS AND VESSELS WITH NUCLEAR POWER UNITS: TASKS AND HARDWARE-METHODICAL SUPPORT

Elastoplastic stresses of a shell of revolution made from the material with linear hardening loaded by a force at the pole

Analysis of edge effects and main stress-strain state of structurally-anisotropic aircraft panels comprising composite materials in refined theory

ANALISIS OF THE “BOUNDARY LAYER“ STRESS-STRAIN STATE IN FRAMES OF THE NONCLASSICAL CYLINDRICAL SHELL THEORY

Suchergebnisse filtern