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  • 1
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    The effect of initial diameter in sperically symmetric droplet combustion of sooting fuels (1994)
    In:  Other Sources
    Details
    Publication Date: 2019-08-28
    Description: The effect of initial droplet diameter on the burning rate of sooting fuels - n-heptane and 1-chloro-octane - was examined experimentally at low gravity. A 1.2s drop tower provided a low gravity environment to minimize buoyancy and achieve spherically symmetric flames for stationary droplets. Free-floating and fiber-supported droplets were burned, and both techniques gave matching results for droplets of similar initial diameter. Burning rate constants for both fuels were measured for a large number of droplets ranging from 0.4 to 1.1mm in initial diameter.
    Keywords: PROPELLANTS AND FUELS
    Type: Royal Society (London) Proceedings, Series A - Mathematical and Physical Sciences (ISSN 0962-8444); 446; 1927; p. 255-276
    Format: text
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    NASA TECHNICAL REPORTS
  • 2
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    Experiments on the effect of initial diameter in spherically symmetric droplet combustion of sooting fuels (1993)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: The effect of initial droplet diameter on the burning rate of sooting fuels (n-heptane and 1-chloro-octane) is studied experimentally at low gravity. A 1.2 s drop tower provided a low gravity environment to minimize buoyancy and achieve spherically symmetric flames for stationary droplets. Free-floating and fiber supported droplets were burned, and both methods gave matching results for droplets of similar initial diameter.
    Keywords: PROPELLANTS AND FUELS
    Type: AIAA PAPER 93-0130 , AIAA, Aerospace Sciences Meeting and Exhibit; Jan 11, 1993 - Jan 14, 1993; Reno, NV; United States|; 19 p.
    Format: text
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    NASA TECHNICAL REPORTS
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