Email RIS file
Bookmark
Report an Issue

Shear coaxial injector atomization phenomena for combusting and non-combusting conditions

Author
Pal, S.
Published
JAN 1, 1992.
Physical Description
1 electronic document
Additional Creators
Moser, M. D., Ryan, H. M., Foust, M. J., and Santoro, R. J.
Online Version

Availability

I Want It
I Want It

Finding items...

Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
Measurements of LOX drop size and velocity in a uni-element liquid propellant rocket chamber are presented. The use of the Phase Doppler Particle Analyzer in obtaining temporally-averaged probability density functions of drop size in a harsh rocket environment has been demonstrated. Complementary measurements of drop size/velocity for simulants under cold flow conditions are also presented. The drop size/velocity measurements made for combusting and cold flow conditions are compared, and the results indicate that there are significant differences in the two flowfields.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19940007054.
Accession ID: 94N11526.
NASA-CR-193339.
NAS 1.26:193339.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15663820