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The use of transonic slender-body theory to calculate the spatial flow over a wing-fuselage configuration - MaRDI portal

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The use of transonic slender-body theory to calculate the spatial flow over a wing-fuselage configuration (Q1264660)

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scientific article; zbMATH DE number 1205655
Language Label Description Also known as
English
The use of transonic slender-body theory to calculate the spatial flow over a wing-fuselage configuration
scientific article; zbMATH DE number 1205655

    Statements

    title
    The use of transonic slender-body theory to calculate the spatial flow over a wing-fuselage configuration (English)
    0 references
    author
    V. V. Negoda
    0 references
    K. G. Sayadyan
    0 references
    publication date
    25 May 1999
    0 references
    zbMATH Keywords
    composite solution
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    potential function
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    perturbed velocity
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    aerodynamic characteristics
    0 references

    Identifiers

    zbMATH DE Number
    1205655
    0 references
     
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