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  • AIRCRAFT  (1)
  • PROPELLANTS AND FUELS  (1)
  • 1
    facet.materialart.
    Unknown
    In:  Other Sources
    Publication Date: 2011-12-21
    Description: The burning behavior of pressed binderless HMX laterally confined in 6.4 mm i.d. steel cases was measured over the pressure range 1.45 to 338 MPa in a constant pressure strand burner. The measured regression rates are compared to those reported previously for unconfined samples. It is shown that lateral confinement results in a several-fold decrease in the regression rate for the coarse particle size HMX above the transition to super fast regression. For class E samples, confinement shifts the transition to super fast regression from low pressure to high pressure. These results are interpreted in terms of the previously proposed progressive deconsolidation mechanism. Preliminary holographic photography and closed bomb tests are also described. Theoretical one dimensional modeling calculations were carried out to predict the expected flame height (particle burn out distance) as a function of particle size and pressure for binderless HMX burning by a progressive deconsolidation mechanism.
    Keywords: PROPELLANTS AND FUELS
    Type: NASA. Langley Res. Center The 17th JANNAF Combust. Meeting, Vol. 2,; p 413-429
    Format: text
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  • 2
    facet.materialart.
    Unknown
    In:  CASI
    Publication Date: 2019-06-27
    Description: The acoustic field generated by a circular jet in the presence of a low speed crossflow is calculated. The solution is obtained for a quadrupole source located in a uniformly moving acoustic medium. Ribner's work on straight jets is used to model the flow in the turbulent crossflow jet. The movement of the acoustic medium results in the acoustic intensity being greater upstream of the jet flow than at an equal distance downstream. A summary is also presented of the analysis for the acoustic intensity of a crossflow jet which is in motion through a stationary acoustic medium. The analysis is applicable to the noise generated by the lift jet of a V/STOL aircraft under take-off or landing conditions. The results of these two configurations provide a comparision of the directional distribution of acoustic intensity measured in a wind tunnel test of a crossflow jet and in a corresponding flight test.
    Keywords: AIRCRAFT
    Type: NASA-CR-2169
    Format: application/pdf
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