2 edition of On the effect of boundary layer growth on the stability of compressible flows found in the catalog.
On the effect of boundary layer growth on the stability of compressible flows
Nabil M El-Hady
1981 by National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service] in Washington, D.C, [Springfield, Va .
Written in English
|Statement||Nabil M. El-Hady ; prepared for Langley Research Center under grant NSG-1645|
|Series||NASA contractor report -- 3474|
|Contributions||United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Langley Research Center|
|The Physical Object|
|Pagination||44 p. :|
|Number of Pages||44|
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Introduction. Linear stability of the flat plate boundary layer flow is a classical flow problem, which has been fully studied by researchers. 1 The numerical solution obtained via solving the Orr-Sommerfeld stability equation is useful and reliable1, 2, 3 in describing the characteristics of an initial stage of boundary layer transition.
The neutral curve of the flat plate boundary layer. Hydrodynamic boundary layer stability. We now turn our attention to another important aspect of boundary layer research; boundary layer stability [18,19]. The most important feature of flow stability analysis is in the value of the growth increment of the unstable disturbances.
A brief discussion of some aspects is discussed. N2 - This paper presents a new numerical method for investigating the relationship between cone nosetip bluntness on boundary layer transition in hypersonic flows. For years, Linear Stability Theory (LST) and the Parabolized Stability Equations (PSE) have provided the tools for analysis and prediction of laminar to turbulent transition for.
Scribd is the world's largest social reading and publishing site. Boundary layer equations (just like the thin-layer Navier-Stokes equations) are based on the notion that at large enough Reynolds numbers, the effects of viscosity are only limited to a small region of the flow: the boundary layer.
The boundary layer and some of its properties are shown in Figure.