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  • ACOUSTICS  (2)
  • Chemistry  (1)
  • 1
    Electronic Resource
    Electronic Resource
    Stamford, Conn. [u.a.] : Wiley-Blackwell
    Polymer Engineering and Science 14 (1974), S. 50-57 
    ISSN: 0032-3888
    Keywords: Chemistry ; Chemical Engineering
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics , Physics
    Notes: The chemo-rheological behavior has been elucidated for three high temperature epoxy resins. Constant temperature and shear stress measurements were made on a modified Weissenberg Rheogoniometer. Curing behavior of various temperatures is unified by a time-temperature superposition method. The curing rate of one resin, Ferro E-293, is limited by the chemical reaction. The other resins, 3M PR-286 and PR-288, each have consecutively occurring reactions, both of which are diffusion limited. The chemo-rheological information obtained for these materials is used to model viscosity for compression molding of hand-laidup composites.
    Additional Material: 15 Ill.
    Type of Medium: Electronic Resource
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  • 2
    Publication Date: 2016-06-07
    Description: The problem of establishing the state of the technology is approached by first identifying the various characteristics of rotor noise and then assessing the state of technology in understanding and predicting the most important of these rotor noise characteristics in a real-world environment.
    Keywords: ACOUSTICS
    Type: NASA. Langley Res. Center Helicopter Acoustics Pt. 2; p 723-780
    Format: application/pdf
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  • 3
    Publication Date: 2019-07-13
    Description: The results of a recent wind tunnel test program to evaluate the effectiveness of the Tip Air Mass Injection (TAMI) system in modifying the blade tip vortex occurring during helicopter flight is described with attention to the effect of this modification on the impulsive noise. The measurement program is explained, and the correlation between experimental and predicted results is discussed. Topics considered include the effect of descent rate on noise pressure time histories, the effect of air mass injection on noise, and the analysis based on a dB(A) weighted approach. Impulsive noise generated by the interaction of a helicopter rotor blade and the concentrated tip vortex during forward flight descent is a primary contributor to acoustic annoyance as it draws early attention to the presence of the helicopter.
    Keywords: ACOUSTICS
    Type: AIAA PAPER 77-1341 , Aeroacoustics Conference; Oct 03, 1977 - Oct 05, 1977; Atlanta, GA
    Format: text
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