NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Effects of AP particle size on combustion response to crossflowAn analytical model is developed for the linearized velocity-coupled combustion response function. The model treats elements of response to perturbations in pressure, in composition due to the heterogeneity of composite propellants, and in crossflow velocity. The effects of AP particle size are accounted for in terms of effects on controlling ballistics properties and in terms of fluctuations in propellant composition. There are two facets of the crossflow problem: the effect of crossflow velocity on the various response elements, and the response to velocity perturbations. Both are dealt with in this paper. Important trends derived from series of parametric computations are described.
Document ID
19830055099
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cohen, N. S.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena; Cohen Professional Services, Inc. Redlands, CA, United States)
Strand, L. D.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena CA, United States)
Date Acquired
August 11, 2013
Publication Date
June 1, 1983
Subject Category
Propellants And Fuels
Report/Patent Number
AIAA PAPER 83-1270
Accession Number
83A36317
Distribution Limits
Public
Copyright
Other

Available Downloads

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