Spacelab Experiments on Combustion of Heptane/Hexadecane Droplets
Abstract
Results are presented from experiments on reduced-gravity combustion of individual heptane/hexadecane droplets. Initial droplet diameters ranged from 0.25 to 5.2 mm, and initial hexadecane mass fractions in the droplets were 0.058, 0.10, 0.20, and 0.40. Most droplets were burned in cabin air on Spacelab with an ambient oxygen mole fraction of about 0.21 and a pressure of about 0.1 MPa. Data were also obtained for small (0.25-mm) droplets in a...
Paper Details
Title
Spacelab Experiments on Combustion of Heptane/Hexadecane Droplets
Published Date
Jan 1, 2001
Journal
Volume
39
Issue
12
Pages
2327 - 2335
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