Isbn: 9789024737536 - virtual principles in aircraft structures: 6-7 (3 risultati)

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  • Lingua: Inglese

    Editore: Springer, 1989

    9024737532 / 9789024737536

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    Da: Anybook.com, Lincoln, Regno UnitoAnybook.com

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    Condizione: Usato - Discreto

    EUR 97,35

    EUR 40,90 spedizione 
    Spedito da Regno Unito a U.S.A.

    Quantità: 1 disponibile

    Condizione: Fair. Volumes 1 & 2. Hardback covers. Ex-library, With usual stamps and markings, In fair condition, suitable as a study copy. No dust jacket. Please note the Image in this listing is a stock photo and may not match the covers of the actual item,1650grams, ISBN:9024737532.

  • Lingua: Inglese

    Editore: Kluwer Academic Pub, 1989

    9024737532 / 9789024737536

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    Da: Libreria sottomarina - Studio Bibliografico, ROMA, RM, ItaliaLibreria sottomarina - Studio Bibliografico

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    Condizione: Usato

    EUR 94,00

    EUR 42,00 spedizione 
    Spedito da Italia a U.S.A.

    Quantità: 1 disponibile

    rilegato. Condizione: Perfetto (Mint). Book.

  • Lingua: Inglese

    Editore: Springer, 1989

    9024737532 / 9789024737536

    • Rilegato

    Da: Buchpark, Trebbin, GermaniaBuchpark

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    Condizione: Usato - Molto buono

    EUR 92,81

    EUR 105,00 spedizione 
    Spedito da Germania a U.S.A.

    Quantità: 2 disponibili

    Condizione: Gut. Zustand: Gut | Seiten: 695 | Sprache: Englisch | Produktart: Bücher | The basic partial differential equations for the stresses and displacements in clas­ sical three dimensional elasticity theory can be set up in three ways: (1) to solve for the displacements first and then the stresses; (2) to solve for the stresses first and then the displacements; and (3) to solve for both stresses and displacements simultaneously. These three methods are identified in the literature as (1) the displacement method, (2) the stress or force method, and (3) the combined or mixed method. Closed form solutions of the partial differential equations with their complicated boundary conditions for any of these three methods have been obtained only in special cases. In order to obtain solutions, various special methods have been developed to determine the stresses and displacements in structures. The equations have been reduced to two and one dimensional forms for plates, beams, and trusses. By neglecting the local effects at the edges and ends, satisfactory solutions can be obtained for many case~. The procedures for reducing the three dimensional equations to two and one dimensional equations are described in Chapter 1, Volume 1, where the various approximations are pointed out.…