Advanced, Small High-Temperature-Rise Combustor Program.

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Abstract:

The objectives of the program were to develop and validate an analytical design technique for high-temperature-rise, low-airflow combustors and related components and to define the limitations associated with these small combustors and related components and the effect of these limitations on the cycle and configuration of advanced-technology engines. Author

Author(s):
No Author(s) Identified
Author Organization(s):
AIRESEARCH MFG CO OF ARIZONA PHOENIX
Descriptive Note:
Semiannual progress rept. 1 Oct 70-31 Mar 71.
Supplementary Note:
See also Rept. no. PE-8120-R3 dated 15 Oct 70, AD-876 447.
Pagination:
0182

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
PE-8120-R9-Rev-1
Contract/Grant Number(s):
DAAJ02-70-C-0060
 Subject Terms
Joint Capability Areas:
JCA_5.3_Planning; JCA_5_Command and Control
Communities of Interest:
No COI(s) Identified
Descriptor(s):
*COMBUSTION CHAMBERS, *GAS TURBINES, COMBUSTION CHAMBERS, FUEL INJECTION, FUEL BURN UP, IGNITION, THERMAL RADIATION, MATHEMATICAL MODELS, STRESSES, MATERIALS
Field(s)/Group(s):
Combustion and Ignition, Jet and Gas Turbine Engines
Report Date:
1971 May 18