Initial-value problem for three-dimensional disturbances in a hypersonic boundary layer

Eric Forgoston, Anatoli Tumin

    Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

    1 Scopus citations

    Abstract

    An initial-value problem is formulated for a threedimensional wave packet in a hypersonic boundary layer flow. The problem is solved using a Laplace transform with respect to time and Fourier transforms with respect to the streamwise and spanwise coordinates. The solution can be presented as a sum of modes consisting of continuous and discrete spectra of temporal stability theory. Two discrete modes, known as Mode S and Mode F, are of interest since they may be involved in a laminar-turbulent transition scenario. The continuous and discrete spectrum are analyzed numerically, and the following features are revealed: (1) the synchronism of Mode S with acoustic waves at low wave number is primarily twodimensional; (2) at high angles of dis turbance propagation, Mode F is no longer synchronized with entropy and vorticity waves; (3) at high angles of disturbance propagation, the synchronism between Mode S and Mode F no longer leads to a Mode S instability, and at even higher angles of disturbance propagation, Mode S and Mode F are not synchronized.

    Original languageEnglish
    Title of host publication34th AIAA Fluid Dynamics Conference and Exhibit
    PublisherAmerican Institute of Aeronautics and Astronautics Inc.
    ISBN (Print)9781624100314
    DOIs
    StatePublished - 2004
    Event34th AIAA Fluid Dynamics Conference and Exhibit 2004 - Portland, OR, United States
    Duration: 28 Jun 20041 Jul 2004

    Publication series

    Name34th AIAA Fluid Dynamics Conference and Exhibit

    Other

    Other34th AIAA Fluid Dynamics Conference and Exhibit 2004
    Country/TerritoryUnited States
    CityPortland, OR
    Period28/06/041/07/04

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