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  • 1970-1974  (4)
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  • 1
    Electronic Resource
    Electronic Resource
    Oxford, UK : Blackwell Publishing Ltd
    Journal of food science 39 (1974), S. 0 
    ISSN: 1750-3841
    Source: Blackwell Publishing Journal Backfiles 1879-2005
    Topics: Agriculture, Forestry, Horticulture, Fishery, Domestic Science, Nutrition , Process Engineering, Biotechnology, Nutrition Technology
    Notes: Tenderization of meat by papaya latex preparations was achieved by the combined action of several proteases. Both in vitro and in vivo application of enzymes gave degradation of muscle proteins, and degradation of connective tissue only after heat denaturation. Purified papaya enzymes-papain, chymopapain and papaya peptidase A-were uniformly distributed throughout the various muscles and in the extravascular system after antemortem injection into the vascular system. Chymopapain was the primary contributor for tenderization because it constituted the major protease in the mixture and it had higher thermostability and more favorable action at the meat's natural pH than papain or papaya peptidase A.
    Type of Medium: Electronic Resource
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  • 2
    Publication Date: 2019-06-27
    Description: Flutter boundaries, as well as flutter limit cycle amplitudes, frequencies and stresses were computed for a panel of length-width ratio 4.48 exposed to applied in-plane and transverse loads. The Mach number range was 1.1 to 1.4. The method used involved direct numerical integration of modal equations of motion derived from the nonlinear plate equations of von Karman, coupled with linearized potential flow aerodynamic theory. The flutter boundaries agreed reasonably well with experiment, except when the in-plane loading approached the buckling load. Structural damping had to be introduced, to produce frequencies comparable to the experimental values. Attempts to compute panel deflections or stress at a given point met with limited success. There is some evidence, however, that deflection and stress maxima can be estimated with somewhat greater accuracy.
    Keywords: AERODYNAMICS
    Type: NASA-CR-120105 , AMS-1116
    Format: application/pdf
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  • 3
    Publication Date: 2019-06-27
    Description: This experimental investigation tested the accuracy of an analysis which predicts the natural frequencies of vibration of a plate constrained by an arbitrary number of point supports along the edges, and also determined the number of such supports which approximates an infinite number.
    Keywords: STRUCTURAL MECHANICS
    Type: NASA-CR-138681 , AMS-1133
    Format: application/pdf
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  • 4
    Publication Date: 2019-07-13
    Description: The in-plane edge impact of composite plates, with or without a protection strip, is investigated. A computational analysis based on the Fast Fourier Transform technique is presented. The particular application of the present method is in the understanding of the foreign object damage problem of composite fan blades. The method is completely general and may be applied to the study of other stress wave propagation problems in a half space. Results indicate that for the protective strip to be effective in reducing impact stresses in the composite the thickness must be equal or greater than the impact contact dimension. Large interface shear stresses at the strip - composite boundary can be induced under impact.
    Keywords: STRUCTURAL MECHANICS
    Type: NASA-CR-134720 , AMS-1141
    Format: application/pdf
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