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  • Other Sources  (3)
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  • 1
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    Studies in Thermocapillary Convection of the Marangoni-Benard Type (1996)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Description: The effects of imposed nonlinear oscillatory shear upon the onset of Marangoni-Bernard convection, as predicted by linear theory, in a layer of liquid with a deformable free surface were reported upon by Or and Kelly for small amplitude oscillations. Depending on the operating conditions, either stabilization or destabilization might occur. The aim of the current paper is to report the results for finite amplitude imposed oscillations so that the actual amount of stabilization or destabilization can be determined for prescribed operating conditions.
    Keywords: Fluid Mechanics and Heat Transfer
    Type: Third Microgravity Fluid Physics Conference; 295-299; NASA-CP-3338
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 2
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    Stabilization of thermocapillary convection by means of nonplanar flow oscillations (1994)
    In:  CASI
    Details
    Publication Date: 2013-08-31
    Description: Nonplanar flow oscillations have been shown to be effective in stabilizing buoyancy-induced Rayleigh-Benard convection. The present study was initiated to see if thermocapillary convection of the Marangoni type might also be stabilized by the same means. When surface deflection can be ignored, significant stabilization occurs. However, when the operating parameters are such that surface deflection is nonnegligible, destabilization can occur, in contrast to Rayleigh-Benard convection. Mechanisms for both stabilization and destabilization are discussed.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: NASA. Lewis Research Center, Second Microgravity Fluid Physics Converence; p 15-20
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 3
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    On the transfer of energy to an unstable liquid jet in a coflowing compressible airstream (1993)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: The transfer of energy from a compressible airstream to a coflowing unstable liquid jet via the pressure perturbation at the interface is studied as the Mach number varies continuously from subsonic to supersonic values. The 'lift' component of the pressure perturbation has been demonstrated to predominate up to slightly supersonic free-stream Mach numbers, after which the 'drag' component predominates.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: Physics of Fluids A (ISSN 0899-8213); 5; 5; p. 1273, 1274.
    Format: text
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    NASA TECHNICAL REPORTS
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