Nikolayev Vladimir (9 results)

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  • Published by Progress Publishers, Moscow, 1984

    • Softcover

    Seller: Goulds Book Arcade, Sydney, Newtown, Sydney, NSW, AustraliaGoulds Book Arcade, Sydney

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    Paper Back. Condition: Very Good. This is the 1984 English translation by Dudley Hagan. 261 pages. The book is a little worn, tanned and creased. 261 pages. Books listed here are not stored at the shop. Please contact us if you want to pick up a book from Newtown. Size: Size D: 7"-8" Tall (177-203mm).…

  • Language: English

    Published by LAP LAMBERT Academic Publishing, 2017

    3330053208 / 9783330053205

    • Softcover

    Seller: Books Puddle, Woodside, NY, U.S.A.Books Puddle

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  • Language: English

    Published by LAP LAMBERT Academic Publishing, 2017

    3330053208 / 9783330053205

    • Softcover

    Seller: moluna, Greven, Germanymoluna

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  • Language: English

    Published by LAP LAMBERT Academic Publishing, 2017

    3330053208 / 9783330053205

    • Softcover

    Seller: preigu, Osnabrück, Germanypreigu

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    Taschenbuch. Condition: Neu. Heat Condition Compartments Of Aircraft With A Honeycomb Structure | Vladimir Nikolayev (u. a.) | Taschenbuch | 132 S. | Englisch | 2017 | LAP LAMBERT Academic Publishing | EAN 9783330053205 | Verantwortliche Person für die EU: BoD - Books on Demand, In de Tarpen 42, 22848 Norderstedt, info[at]bod[dot]de | Anbieter: preigu. …

  • Language: English

    Published by LAP LAMBERT Academic Publishing, 2017

    3330053208 / 9783330053205

    • Softcover

    Seller: Revaluation Books, Exeter, United KingdomRevaluation Books

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    Paperback. Condition: Brand New. 132 pages. 8.66x5.91x0.30 inches. In Stock.

  • Language: English

    Published by LAP LAMBERT Academic Publishing Mrz 2017, 2017

    3330053208 / 9783330053205

    • Softcover
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    Seller: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, GermanyBuchWeltWeit Ludwig Meier e.K.

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    Taschenbuch. Condition: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -A theoretical method of mathematical simulation of the long-range aircraft compartments and systems thermal state are developed. To solve the direct problem, i.e. for stiff nonlinear differential equations solving, the implicit Rosenbrock method of second-order for non-autonomous systems is used. In solving the direct problem of the compartments thermal state for honeycomb core constructions the developed algorithm using a parabolic boundary value problem with discontinuous coefficients based on the numerical solution of stochastic differential equations is applied. In solving inverse problems for multidimensional heat conduction equations the developed technique with the use of derivatives assessments on the functional parameters of the expected diffusion processes is applied. As the algorithms of parametric identification of the aircraft compartments and systems thermal state model in the form of ordinary differential equations the quasi-Newton method of Broyden-Fletcher-Goldfarb-Shenno combined with the Newton's method is proposed. 132 pp. Englisch.…

  • Language: English

    Published by LAP LAMBERT Academic Publishing, 2017

    3330053208 / 9783330053205

    • Softcover
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    Seller: Majestic Books, Hounslow, United KingdomMajestic Books

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  • Language: English

    Published by LAP LAMBERT Academic Publishing, 2017

    3330053208 / 9783330053205

    • Softcover
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    Seller: Biblios, frankfurt am main, HESSE, GermanyBiblios

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    Condition: New. PRINT ON DEMAND.

  • Language: English

    Published by LAP LAMBERT Academic Publishing Mär 2017, 2017

    3330053208 / 9783330053205

    • Softcover
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    Seller: buchversandmimpf2000, Emtmannsberg, BAYE, Germanybuchversandmimpf2000

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    Taschenbuch. Condition: Neu. This item is printed on demand - Print on Demand Titel. Neuware -A theoretical method of mathematical simulation of the long-range aircraft compartments and systems thermal state are developed. To solve the direct problem, i.e. for stiff nonlinear differential equations solving, the implicit Rosenbrock method of second-order for non-autonomous systems is used. In solving the direct problem of the compartments thermal state for honeycomb core constructions the developed algorithm using a parabolic boundary value problem with discontinuous coefficients based on the numerical solution of stochastic differential equations is applied. In solving inverse problems for multidimensional heat conduction equations the developed technique with the use of derivatives assessments on the functional parameters of the expected diffusion processes is applied. As the algorithms of parametric identification of the aircraft compartments and systems thermal state model in the form of ordinary differential equations the quasi-Newton method of Broyden-Fletcher-Goldfarb-Shenno combined with the Newton's method is proposed.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 132 pp. Englisch.…