PL EN


Preferencje help
Widoczny [Schowaj] Abstrakt
Liczba wyników
2013 | 13 | 4 |
Tytuł artykułu

Stress-strain analysis of metal butt connection with composite propeller blade

Treść / Zawartość
Warianty tytułu
RU
Analiz kharakteristik lokal'nogo naprjazhenno-deformirovannogo sostajanija sojedinenija metallicheskogo komlja s kompozitnojj lopast'ju vozdushnogo vinta
Języki publikacji
EN
Abstrakty
EN
RU
Wydawca
-
Rocznik
Tom
13
Numer
4
Opis fizyczny
p.143-148,fig.,ref.
Twórcy
autor
  • Volodymyr Dahl East-Ukrainian National University, Molodizhny bl., 20a, Lugansk, 91034, Ukraine
autor
  • Volodymyr Dahl East-Ukrainian National University, Molodizhny bl., 20a, Lugansk, 91034, Ukraine
autor
  • Volodymyr Dahl East-Ukrainian National University, Molodizhny bl., 20a, Lugansk, 91034, Ukraine
Bibliografia
  • Chumachenko E.I., Polyakova T.V., Aksenov S.A., 2009.: Mathematical modeling of non-linear mechanics (Overview of software systems to meet the challenges of modeling complex systems) - M.: Institute for Space Research RAN. - 43. (in Russian).
  • Djur E.O., Kuchma L.D., Manko T.A., 2003.: Polymer composites in rocket and space technology: textbook - K.: Higher education. - 399. (in Ukrainian).
  • Gagauz F.M., Gumennikov V.V., 2013.: Simulation parameters composite structural connecting element / Issues of design and production of aircraft constructions: Scientific journal of National Aerospace University «KHAI». -2 (74). - Kh., 46-53. (in Russian).
  • Gladkiy I.L., 2004.: Investigating the effects of failure blades of aircraft engines by finite element method // Vibrations in engineering and technologies. - N°5 (37). - 38-41. (in Russian).
  • ISO 9809-2:2000 (E)., 2006.: Gas Cylinders - Refillable Seamless Steel Gas Cylinders - Design, Construction and Testing. Part 2: Quenched and Tempered Steel Cylinders with Tensile Strength Greater than or Equal to 1100 MPa. International Standard. ISO.
  • Jakovenko P.Ja., Malkov I.V., Korbach V.G., Syrovoy G.V., 2013.: Simulation of shock loading of metal-cylindrical shells with a partial reinforcement // Open information and computer integrated technologies. Collection of scientific works of the National Aerospace University named after N.E. Zhukovsky, «KHAI» - Kh., N° 58. - 73-80. (in Russian).
  • Karpov Y.S., 2006.: Compound parts and units of composite materials - Kn.: National aerospace university " Kharkov aviation institute". - 359. (in Russian).
  • Karpov Y.S., 2010.: The design of parts and assemblies made of composites. National aerospace university " Kharkov aviation institute", Kh. - 768. (in Russian).
  • Kharchenko M.E., 2013.: The approximate relationship between the tensile strengths of polymer composite materials in compression, tension and bending // Issues of design and production of aircraft constructions: Scientific journal of National Aerospace University «KHAI». -2 (74). - Kh., 54-63. (in Russian).
  • Kovalenko V.A., Kondratev A.V., 2011.: The use of polymer composite materials in products of rocket and space technology as a reserve for increasing its mass and functional efficiency // Aerospace engineering and technology. - N° 5 (82). - 14-20. (in Russian).
  • Malkov I.V., Bondar L., Makukhin A.G., Syrovoj G.V., 2010.: Properties of epoxy materials with different nano-modifiers // TEKA. Commission of motorization and power industry in agriculture Lublin university of texnology. Lublin - 28-32.
  • Malkov I.V., Bondar L., Makukhin A.G., Syrovoj G.V., 2010.: Effect ofnanomodification on durability of adhesive joint of polymeric composite materials // TEKA. Commission of motorization and power industry in agriculture Lublin university of texnology. Lublin. - 185189.
  • Malkov I.V., Sirovoy G.V., Kashkarov S.A., Nepran. I.L., 2013.: Comparative analysis of the simulation and calculation of the mechanical properties of articles made of composite materials in SolidWorks - Scientific journal of East Ukrainian National University. Krasnodon: EUNU named after V. Dahl. (in Russian).
  • Malkov I.V., Sirovoy G.V., Kashkarov S.A., Nepran. I.L., 2012.: The analysis of adhesion effect on properties of the modified polymeric nano composites, - TEKA Vol. 12 N. 4.
  • Malkov I.V., Sirovoy G.V., Kashkarov S.A., Nepran. I.L., 2012.: The calculation method of small-sized composite enclosures in CAD/CAE systems - TEKA Vol. 12 N. 3
  • Malkov I.V., Syrovoy G.V., Nepran I.L., 2010.: Analysis of descriptions local tensely the deformatione states fortune of connection compound of metallic flange with a composite corps. Open information and computer integrated technologies // Collection of scientific works of the National Aerospace University of N.E. Zhukovsky, «KHAI» - Kh., 48. - 80-86. (in Russian).
  • NASA, 20.06.2011.: Composite Crew Module FiberSIM [Electronic resource]. - http:// www.vistagy.com.
  • Nosko P., Breshev V., Fil P., Boyko G., 2010.: Structural synthesis and design variants for noncontact machine drives. TEKA Commission of Motorization and Power Industry in Agriculture, OL RAN, IOB. 77-86.
  • Polinovskiy V.P., 2003.: Application software by MSC. Software for the calculation of new products from composite materials [Electronic resource] / Rus. conf. users of MSC - M.: MSC. Software Corporation. http://www.mscsoftware.ru/document/conf/Mosco w_conf/conf_2003/ khntn2.zip. - 07.06.2011. (in Russian).
  • Troschenko V.T., Lebedev A.A., Strijalo V.A., Stepanov G.V., Krivenyuk V.V., 2000.: )Mechanical behavior of materials under different types of loading. - K. - 566. (in Russian).
  • Vorobiev Yu.S., Chernobryvko M.V., 2004.: Nonlinear high-strain-rate elastic-plastic deformation of structural elements under impulsive loading [Text] // the Int. Conf. on Nonlinear Dynamics. - Kharkov, September 1416. - 164-167.
  • Vorobiev Ju.S., Chernobryvko M.V., Kushka L., 2005.: Local pulsed effect on shell elements structures // Aerospace engineering and technology. - N° 9 (25). - 181-184. (in Russian)
Typ dokumentu
Bibliografia
Identyfikatory
Identyfikator YADDA
bwmeta1.element.agro-554223a5-bc4b-44db-a6de-4e0a22ea032c
JavaScript jest wyłączony w Twojej przeglądarce internetowej. Włącz go, a następnie odśwież stronę, aby móc w pełni z niej korzystać.