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  • 1
    Publication Date: 2019-07-13
    Description: A self-consistent scheme for relating wind tunnel ice accretion roughness to the resulting enhancement of heat transfer is described. First, a spectral technique of quantitative analysis of early ice roughness images is reviewed. The image processing scheme uses a spectral estimation technique (SET) which extracts physically descriptive parameters by comparing scan lines from the experimentally-obtained accretion images to a prescribed test function. Analysis using this technique for both streamwise and spanwise directions of data from the NASA Lewis Icing Research Tunnel (IRT) are presented. An experimental technique is then presented for constructing physical roughness models suitable for wind tunnel testing that match the SET parameters extracted from the IRT images. The icing castings and modeled roughness are tested for enhancement of boundary layer heat transfer using infrared techniques in a "dry" wind tunnel.
    Keywords: Fluid Mechanics and Heat Transfer
    Type: NASA/CR-96-112616 , NAS 1.26:112616 , AIAA Paper 96-0865 , Aerospace Sciences Meeting and Exhibit; Jan 15, 1996 - Jan 19, 1996; Reno, NV; United States
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  • 2
    Publication Date: 2019-08-16
    Description: An experimental method is described to measure and compare the convective heat transfer coefficient of natural and simulated ice accretion roughness and to provide a rational means for determining accretion-related enhanced heat transfer coefficients. The natural ice accretion roughness was a sample casting made from accretions at the NASA Lewis Icing Research Tunnel (IRT). One of these castings was modeled using a Spectral Estimation Technique (SET) to produce three roughness elements patterns that simulate the actual accretion. All four samples were tested in a flat-plate boundary layer at angle of attack in a "dry" wind tunnel test. The convective heat transfer coefficient was measured using infrared thermography. It is shown that, dispite some problems in the current data set, the method does show considerable promise in determining roughness-induced heat transfer coefficients, and that, in addition to the roughness height and spacing in the flow direction, the concentration and spacing of elements in the spanwise direction are important parameters.
    Keywords: Fluid Mechanics and Heat Transfer
    Type: NASA/CR-97-112617 , NAS 1.26:112617 , AIAA Paper 97-1018 , Aerospace Sciences Meeting and Exhibit; Jan 06, 1997 - Jan 10, 1997; Reno, NV; United States
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