DYNAMICS OF TWO-PHASE FLOW IN ROCKET NOZZLES

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Abstract:

No Abstract Identified

Author(s):
Wrenn, B. G. ; Dunlap, R.
Author Organization(s):
UNITED TECHNOLOGY CENTER SUNNYVALE CALIF
Annotation:
AN INVESTIGATION IS REPORTED OF NOZZLE FLOW DYNAMICS OF THE GAS-PARTICLE MIXTURE PRODUCED BY COMBUSTION OF SOLID ROCKET PROPELLANTS CONTAINING METAL ADDITIVES.
Pagination:
0059

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
2005 QT4
Contract/Grant Number(s):
NOw-61-0760
 Subject Terms
Joint Capability Areas:
JCA_3.2_Engagement; JCA_3_Force Application
Communities of Interest:
No COI(s) Identified
Descriptor(s):
*COMBUSTION CHAMBER GASES, *EXHAUST GASES, *SOLID ROCKET PROPELLANTS, AERODYNAMIC CHARACTERISTICS, COMBUSTION, DRAG, EQUATIONS, FLUID FLOW, FUEL ADDITIVES, GAS FLOW, MATHEMATICAL ANALYSIS, METALS, MODEL TESTS, PARTICLES, ROCKET NOZZLES, SPHERES, VELOCITY
Report Date:
1962 May 26