HIGH BYPASS RATIO PROPULSION SYSTEMS INVESTIGATION.

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Abstract:

Performance results of logistics transport type advanced high bypass ratio turbofan propulsion systems are reported in terms of SFC and FnWa as well as in terms of relative aircraft range for a range of engine bypass ratios, cycle pressure ratios, and turbine inlet temperatures. Engine weight study results from the application of advanced materials and results of control system studies are also reported. Utilizing the propulsion data, aircraft cost effectiveness analysis and off-design mission analysis were performed and are reported. Author

Author(s):
No Author(s) Identified
Author Organization(s):
GENERAL ELECTRIC CO CINCINNATI OHIO ADVANCED TECHNOLOGY AND DEMONSTRATOR PROGRAMS DEPT
Descriptive Note:
Final rept. Aug 65-Aug 66.
Pagination:
0228

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release
Distribution Statement:
Approved For Public Release; Distribution Unlimited.

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
AFAPL-TR-66-112
Contract/Grant Number(s):
AF 33(615)-2894
Monitor Series:
TR-66-112
 Subject Terms
Joint Capability Areas:
JCA_5.3_Planning; JCA_5_Command and Control
Communities of Interest:
Air Platforms
Descriptor(s):
*TURBOFAN ENGINES, PERFORMANCE(ENGINEERING), LOGISTICS, AIR TRANSPORTATION, FUEL CONSUMPTION, WEIGHT, MISSION PROFILES, ERRORS, THERMODYNAMICS, COST EFFECTIVENESS, HYDROGEN, JET TRANSPORT AIRCRAFT, JET ENGINE FUELS, DRAG, HEAT EXCHANGERS
Field(s)/Group(s):
Jet and Gas Turbine Engines
Keyword(s):
BYPASS RATIO
Report Date:
1966 Nov 01