Streamwise vortices in heated boundary layers. Final Report
Technical Report
·
OSTI ID:7252621
The nonlinear instability of the boundary layer on a heated flat plate placed in an oncoming flow is investigated. Such flows are unstable to stationary vortex instabilities and inviscid traveling wave disturbances governed by the Taylor-Goldstein equation. For small temperature differences the Taylor-Goldstein equation reduces to Rayleigh's equation. When the temperature difference between the wall and free stream is small the preferred mode of instability is a streamwise vortex. It is shown in this case that the vortex, assumed to be of small wavelength, restructures the underlying mean flow to produce a profile which can be massively unstable to inviscid traveling waves. The mean state is shown to be destabilized or stabilized to inviscid waves depending on whether the Prandtl number is less or greater than unity.
- Research Organization:
- National Aeronautics and Space Administration, Hampton, VA (United States). Inst. for Computer Applications in Science and Engineering
- OSTI ID:
- 7252621
- Report Number(s):
- N-92-29692; NASA-CR--189661; NAS--1.26:189661; ICASE--92-23; CNN: NAS1-18605; RTOP 505-90-52-01
- Country of Publication:
- United States
- Language:
- English
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