THERMODYNAMIC CALCULATION OF REACTION-TYPE COMBUSTION CHAMBERS, FUNCTIONING ON A FUEL OF THE TYPE CcHhOoNn WITH A COEFFICIENT OF EXCESS OXIDIZER GREATER THAN 1,

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Abstract:

A method is presented for the thermodynamic calculation of fuel burning at constant pressure. The expansion of the combustion products to a given pressure on the edge of the nozzle takes place isentropically. The authors state that utilization of the proposed method, thermodynamic calculation can be performed with a specified coefficient of excess oxidizer for fuel containing carbon, hydrogen, oxygen, and nitrogen.

Author(s):
Goldaev, I. P. ; Cherepanov, V. P.
Author Organization(s):
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Supplementary Note:
Edited trans. of Samoletostroenie i Tekhnika Vozdushnogo Flota (USSR) n11 p11-16 1967, by V. Mesenzeff.
Annotation:
Thermodynamic calculation of reaction-type combustion chambers, functioning on a fuel of the type CcHhOoNn with a coefficient of excess oxidizer greater than 1--Translation.
Pagination:
0011

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
FTD-HT-23-603-69
 Subject Terms
Communities of Interest:
No COI(s) Identified
Descriptor(s):
(*HYDROCARBONS, *COMBUSTION), (*FUELS, COMBUSTION), THERMODYNAMICS, USSR
Field(s)/Group(s):
Combustion and Ignition
Keyword(s):
TRANSLATIONS
Report Date:
1970 Feb 03