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Supplementary Free-Spinning-Tunnel Tests of a 1/16-Scale Model of the McDonnell Xb-85 Airplane Equipped with a Conventional-Tail Arrangement by Walter J. Klinar, Nasa Technical Reports Server (Ntrs) - Paperback
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Supplementary Free-Spinning-Tunnel Tests of a 1/16-Scale Model of the McDonnell Xb-85 Airplane Equipped with a Conventional-Tail Arrangement by Walter J. Klinar, Nasa Technical Reports Server (Ntrs) - Paperback

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Category Type
Politics
ISBN
9781287265399
Author
Walter J. Klinar, Nasa Technical Reports Server (Ntrs)
Publisher
Bibliogov
Description:

Spin tests have been conducted in the Langley free-spinning tunnel on a 1/16-scale model of the McDonnell XP-85 airplane with the normal X-tail replaced with a short-coupled conventional tail arrangement. The effect of the conventional tail arrangement and the effects of various modifications upon the spin and recovery characteristics of the model were determined. The results of the tests ...

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PRODUCT INFORMATION

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    Specifications

    Category Type
    Politics
    ISBN
    9781287265399
    Item EAN
    2724352846625
    People
    Author
    Walter J. Klinar, Nasa Technical Reports Server (Ntrs)
    People
    Publisher
    Bibliogov
    Category Type
    Politics
    ISBN
    9781287265399
    Item EAN
    2724352846625
    People
    Author
    Walter J. Klinar, Nasa Technical Reports Server (Ntrs)
    People
    Publisher
    Bibliogov
    Technical Information
    Binding
    Paperback
    Languages and countries
    Book Language
    English
    Read more
  •  

    Description:

    Spin tests have been conducted in the Langley free-spinning tunnel on a 1/16-scale model of the McDonnell XP-85 airplane with the normal X-tail replaced with a short-coupled conventional tail arrangement. The effect of the conventional tail arrangement and the effects of various modifications upon

    Spin tests have been conducted in the Langley free-spinning tunnel on a 1/16-scale model of the McDonnell XP-85 airplane with the normal X-tail replaced with a short-coupled conventional tail arrangement. The effect of the conventional tail arrangement and the effects of various modifications upon the spin and recovery characteristics of the model were determined. The results of the tests indicated that installation of the conventional tail arrangement wil not provide satisfactory recoveries from spins of the airplane. Satisfactory recoveries will be obtainable, however, either by installing in addition a very large ventral fin (17.94 sq ft, full-scale) below the tail or by decreasing the width of the fuselage and making it flat sided rearward of the wing trailing edge.

    Product Features:
    • Category: Politics
    • Binding: Paperback
    • Language of Text: English
    • Author(s): Walter J. Klinar, Nasa Technical Reports Server (Ntrs)
    • Publisher: Bibliogov
    • ISBN: 9781287265399
    • Number of Pages: 36
    • Dimensions: 9.69 x 7.44 x 0.07 inches
 

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