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Determination of the Mass Moments and Radii of Inertia of the Sections of a Tapered Wing and the Center-Of-Gravity Line Along the Wing Span by V. V. Savelyev, Nasa Technical Reports Server (Ntrs) - Paperback
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Determination of the Mass Moments and Radii of Inertia of the Sections of a Tapered Wing and the Center-Of-Gravity Line Along the Wing Span by V. V. Savelyev, Nasa Technical Reports Server (Ntrs) - Paperback

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Category Type
Politics
ISBN
9781287264651
Author
V. V. Savelyev, Nasa Technical Reports Server (Ntrs)
Publisher
Bibliogov
Description:

For computing the critical flutter velocity of a wing among the data required are the position of the line of centers of gravity of the wing sections along the span and the mass moments and radii of inertia of any section of the wing about the axis passing through the center of gravity of the section. A sufficiently detailed computation of these magnitudes even if the weights of all the ...

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PRODUCT INFORMATION

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    Specifications

    Category Type
    Politics
    ISBN
    9781287264651
    Item EAN
    2724352844683
    People
    Author
    V. V. Savelyev, Nasa Technical Reports Server (Ntrs)
    People
    Publisher
    Bibliogov
    Category Type
    Politics
    ISBN
    9781287264651
    Item EAN
    2724352844683
    People
    Author
    V. V. Savelyev, Nasa Technical Reports Server (Ntrs)
    People
    Publisher
    Bibliogov
    Technical Information
    Binding
    Paperback
    Languages and countries
    Book Language
    English
    Read more
  •  

    Description:

    For computing the critical flutter velocity of a wing among the data required are the position of the line of centers of gravity of the wing sections along the span and the mass moments and radii of inertia of any section of the wing about the axis passing through the center of gravity of the

    For computing the critical flutter velocity of a wing among the data required are the position of the line of centers of gravity of the wing sections along the span and the mass moments and radii of inertia of any section of the wing about the axis passing through the center of gravity of the section. A sufficiently detailed computation of these magnitudes even if the weights of all the wing elements are known, requires a great deal of time expenditure. Thus a rapid competent worker would require from 70 to 100 hours for the preceding computations for one wing only, while hundreds of hours would be required if all the weights were included. With the aid of the formulas derived in the present paper, the preceding work can be performed with a degree of accuracy sufficient for practical purposes in from one to two hours, the only required data being the geometric dimensions of the outer wing (tapered part), the position of its longerons, the total weight of the outer wing, and the approximate weight of the longerons, The entire material presented in this paper is applicable mainly to wings of longeron construction of the CAHI type and investigations are therefore being conducted by CAHI for the derivation of formulas for the determination of the preceding data for wings of other types.

    Product Features:
    • Category: Politics
    • Binding: Paperback
    • Language of Text: English
    • Author(s): V. V. Savelyev, Nasa Technical Reports Server (Ntrs)
    • Publisher: Bibliogov
    • ISBN: 9781287264651
    • Number of Pages: 32
    • Dimensions: 9.69 x 7.44 x 0.07 inches
 

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