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    Numerical Solutions of Nonsteady Two-Dimensional Transonic Flows

    Source: Journal of Fluids Engineering:;1979:;volume( 101 ):;issue: 003::page 341
    Author:
    M. Couston
    ,
    J. J. Angelini
    DOI: 10.1115/1.3448973
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An alternating-direction implicit algorithm is applied to solve an improved formulation of the low-frequency, small-disturbance, two-dimensional potential equation. Linear solutions are presented for oscillating trailing edge flaps, plunging and pitching flat-plate airfoils, and compared with results obtained by a doublet-lattice-method. Nonlinear calculations for both steady and unsteady flow problems are then compared with results obtained by using the complete Euler equations. The present procedure allows one to solve complex aerodynamic problems, including flows with shock waves.
    keyword(s): Flow (Dynamics) , Shock waves , Algorithms , Equations , Flat plates , Transonic flow , Unsteady flow AND Airfoils ,
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      Numerical Solutions of Nonsteady Two-Dimensional Transonic Flows

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    https://yetl.yabesh.ir/yetl1/handle/yetl/92289
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    • Journal of Fluids Engineering

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    contributor authorM. Couston
    contributor authorJ. J. Angelini
    date accessioned2017-05-08T23:07:00Z
    date available2017-05-08T23:07:00Z
    date copyrightSeptember, 1979
    date issued1979
    identifier issn0098-2202
    identifier otherJFEGA4-26948#341_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/92289
    description abstractAn alternating-direction implicit algorithm is applied to solve an improved formulation of the low-frequency, small-disturbance, two-dimensional potential equation. Linear solutions are presented for oscillating trailing edge flaps, plunging and pitching flat-plate airfoils, and compared with results obtained by a doublet-lattice-method. Nonlinear calculations for both steady and unsteady flow problems are then compared with results obtained by using the complete Euler equations. The present procedure allows one to solve complex aerodynamic problems, including flows with shock waves.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleNumerical Solutions of Nonsteady Two-Dimensional Transonic Flows
    typeJournal Paper
    journal volume101
    journal issue3
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.3448973
    journal fristpage341
    journal lastpage347
    identifier eissn1528-901X
    keywordsFlow (Dynamics)
    keywordsShock waves
    keywordsAlgorithms
    keywordsEquations
    keywordsFlat plates
    keywordsTransonic flow
    keywordsUnsteady flow AND Airfoils
    treeJournal of Fluids Engineering:;1979:;volume( 101 ):;issue: 003
    contenttypeFulltext
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