NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Pressure Effects in Droplet Combustion of Miscible Binary FuelsThe objective of this research is to improve understanding of the combustion of binary fuel mixtures in the vicinity of the critical point. Fiber-supported droplets of mixtures of n-heptane and n-hexadecane, initially 1 mm in diameter, were burned in room-temperature air at pressures from 1 MPa to 6 MPa under free-fall microgravity conditions. For most mixtures the total burning time was observed to achieve a minimum value at pressures well above the critical pressure of either of the pure fuels. This behavior is explained in terms of critical mixing conditions of a ternary system consisting of the two fuels and nitrogen. The importance of inert-gas dissolution in the liquid fuel near the critical point is thereby re-emphasized, and nonmonotonic dependence of dissolution on initial fuel composition is demonstrated. The results provide information that can be used to estimate high-pressure burning rates of fuel mixtures.
Document ID
19970020627
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Masato Mikami
(Yamaguchi University Yamaguchi, Japan)
Osamu Habara
(University of Tokyo Japan)
Michikata Kono
(University of Tokyo Japan)
Jun'ichi Sato
(Ishikawajima-Harima Heavy Industries Co. Ltd. Tokyo, Japan)
Daniel L Dietrich
(Lewis Research Center Cleveland, OH, United States)
Forman A Williams
(University of California San Diego San Diego, United States)
Date Acquired
August 17, 2013
Publication Date
May 1, 1997
Publication Information
Publication: Fourth International Microgravity Combustion Workshop
Publisher: National Aeronautics and Space Administration
Subject Category
Inorganic, Organic and Physical Chemistry
Report/Patent Number
NASA-CP-10194
Meeting Information
Meeting: Fourth International Microgravity Combustion Workshop
Location: Cleveland, OH
Country: US
Start Date: May 19, 1997
End Date: May 21, 1997
Sponsors: National Aeronautics and Space Administration
Accession Number
97N21900
Funding Number(s)
CONTRACT_GRANT: NAG3-1248
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Technical Management
No Preview Available