NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Vaporization and combustion of fuel droplets at supercritical conditionsVaporization and combustion liquid-fuel droplets in both sub- and super-critical environments have been examined. The formulation is based on the complete conservation equations for both gas and liquid phases, and accommodates finite-rate chemical kinetics and a full treatment of liquid-vapor phase equilibrium at the droplet surface. The governing equations and the associated interface boundary conditions are solved numerically using a fully coupled, implicit scheme with the dual time-stepping integration technique. The model is capable of treating the entire droplet history, including the transition from the subcritical to the supercritical state. As a specific example, the combustion of n-pentane fuel droplets in air is studied for pressures of 5-140 atm. In addition, the dynamic responses of droplet vaporization and combustion to ambient-pressure oscillations are investigated. Results indicate that the droplet gasification and burning mechanisms depend greatly on the ambient pressure. In particular, a rapid enlargement of the vaporization and combustion responses occurs when the droplet surface reaches its critical point, mainly due to the strong variations of latent heat of vaporization and thermophysical properties at the critical state.
Document ID
19910067843
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Yang, Vigor
(NASA Propulsion Engineering Research Center; Pennsylvania State University University Park, United States)
Date Acquired
August 14, 2013
Publication Date
September 1, 1991
Subject Category
Inorganic And Physical Chemistry
Report/Patent Number
AIAA PAPER 91-3600
Accession Number
91A52466
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available