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Acoustic Source Modeling for High Speed Air Jets by Marvin E. Goldstein, Abbas Khavaran, Nasa Technical Reports Server (Ntrs) - Paperback
60.90 AED

Acoustic Source Modeling for High Speed Air Jets by Marvin E. Goldstein, Abbas Khavaran, Nasa Technical Reports Server (Ntrs) - Paperback

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60.90 AED 

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Category Type
Politics
ISBN
9781287262732
Author
Marvin E. Goldstein, Abbas Khavaran, Nasa Technical Reports Server (Ntrs)
Publisher
Bibliogov
Description:

The far field acoustic spectra at 90deg to the downstream axis of some typical high speed jets are calculated from two different forms of Lilley s equation combined with some recent measurements of the relevant turbulent source function. These measurements, which were limited to a single point in a low Mach number flow, were extended to other conditions with the aid of a highly developed ...

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PRODUCT INFORMATION

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    Specifications

    Category Type
    Politics
    ISBN
    9781287262732
    Item EAN
    2724352839986
    People
    Author
    Marvin E. Goldstein, Abbas Khavaran, Nasa Technical Reports Server (Ntrs)
    People
    Publisher
    Bibliogov
    Category Type
    Politics
    ISBN
    9781287262732
    Item EAN
    2724352839986
    People
    Author
    Marvin E. Goldstein, Abbas Khavaran, Nasa Technical Reports Server (Ntrs)
    People
    Publisher
    Bibliogov
    Technical Information
    Binding
    Paperback
    Languages and countries
    Book Language
    English
    Read more
  •  

    Description:

    The far field acoustic spectra at 90deg to the downstream axis of some typical high speed jets are calculated from two different forms of Lilley s equation combined with some recent measurements of the relevant turbulent source function. These measurements, which were limited to a single point in a

    The far field acoustic spectra at 90deg to the downstream axis of some typical high speed jets are calculated from two different forms of Lilley s equation combined with some recent measurements of the relevant turbulent source function. These measurements, which were limited to a single point in a low Mach number flow, were extended to other conditions with the aid of a highly developed RANS calculation. The results are compared with experimental data over a range of Mach numbers. Both forms of the analogy lead to predictions that are in excellent agreement with the experimental data at subsonic Mach numbers. The agreement is also fairly good at supersonic speeds, but the data appears to be slightly contaminated by shock-associated noise in this case.

    Product Features:
    • Category: Politics
    • Binding: Paperback
    • Language of Text: English
    • Author(s): Marvin E. Goldstein, Abbas Khavaran, Nasa Technical Reports Server (Ntrs)
    • Publisher: Bibliogov
    • ISBN: 9781287262732
    • Number of Pages: 30
    • Dimensions: 9.69 x 7.44 x 0.06 inches
 

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