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Lateral Oscillatory Characteristics of the Republic F-91 Airplane Calculated by Using Low-Speed Experimental Static and Rotary Derivatives by Byron M. Jaquet, H. S. Fletcher, Nasa Technical Reports Server (Ntrs) - Paperback
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Lateral Oscillatory Characteristics of the Republic F-91 Airplane Calculated by Using Low-Speed Experimental Static and Rotary Derivatives by Byron M. Jaquet, H. S. Fletcher, Nasa Technical Reports Server (Ntrs) - Paperback

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Category Type
Politics
ISBN
9781287265504
Author
Byron M. Jaquet, H. S. Fletcher, Nasa Technical Reports Server (Ntrs)
Publisher
Bibliogov
Description:

The present investigation was conducted to determine, from low-speed tests in the Langley stability tunnel, the static and rotary derivatives of a 1/9-scale model of the Republic F-91 airplane and various of its components (including the effects of wing incidence) and to determine the accuracy with which the period and damping of the lateral oscillation of the airplane could be calculated ...

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PRODUCT INFORMATION

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    Specifications

    Category Type
    Politics
    ISBN
    9781287265504
    Item EAN
    2724352846922
    People
    Author
    Byron M. Jaquet, H. S. Fletcher, Nasa Technical Reports Server (Ntrs)
    People
    Publisher
    Bibliogov
    Category Type
    Politics
    ISBN
    9781287265504
    Item EAN
    2724352846922
    People
    Author
    Byron M. Jaquet, H. S. Fletcher, Nasa Technical Reports Server (Ntrs)
    People
    Publisher
    Bibliogov
    Technical Information
    Binding
    Paperback
    Languages and countries
    Book Language
    English
    Read more
  •  

    Description:

    The present investigation was conducted to determine, from low-speed tests in the Langley stability tunnel, the static and rotary derivatives of a 1/9-scale model of the Republic F-91 airplane and various of its components (including the effects of wing incidence) and to determine the accuracy with

    The present investigation was conducted to determine, from low-speed tests in the Langley stability tunnel, the static and rotary derivatives of a 1/9-scale model of the Republic F-91 airplane and various of its components (including the effects of wing incidence) and to determine the accuracy with which the period and damping of the lateral oscillation of the airplane could be calculated by using these experimentally between flight and calculated period and damping of the lateral oscillation were made for Mach numbers from 0.4 to 0.9 at an altitude of 20, OOO feet for 0deg wing incidence and several other wing incidences. Some comparisons were made of the static and rotary derivatives of the model and derivatives estimated by available procedures. determined derivatives (corrected for Mach number effects). Comparisons The results of the investigation have indicated that the model did not have unusual aerodynamic characteristics except for a large (about -0.125) increment in the damping in yaw contributed by the fuselage. Changes in wing incidence, in general, had little effect on the static and rotary derivatives of the model. The static and rotary derivatives of the model could be estimated with good accuracy only in the low angle-of-attack range by using available procedures.

    Product Features:
    • Category: Politics
    • Binding: Paperback
    • Language of Text: English
    • Author(s): Byron M. Jaquet, H. S. Fletcher, Nasa Technical Reports Server (Ntrs)
    • Publisher: Bibliogov
    • ISBN: 9781287265504
    • Number of Pages: 44
    • Dimensions: 9.69 x 7.44 x 0.09 inches
 

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