High Bypass Turbofan Component Development. Phase II. Detailed Design.

reportActive / Technical Report | Accession Number: ADA082753 | Open PDF

Abstract:

A detailed aerodynamic, aeromechanical and mechanical design of the high bypass turbofan fan stage selected during Phase I of this program was satisfactorily completed. This fan design is the result of aero and aeromechanical iterations and trade-offs which achieved the objectives of meeting aerodynamic performance as well as the life and mechanical considerations of MIL-E-5007D. The resulting fan design compares very closely to the fan originally proposed. Author

Author(s):
Mauch, H. ; Oldakowski, T. ; Weldon, D.
Author Organization(s):
GENERAL ELECTRIC CO LYNN MA AIRCRAFT ENGINE GROUP
Descriptive Note:
Interim technical rept. 4 Oct 78-25 May 79,
Supplementary Note:
See also Phase 1, AD-B041 614L.
Pagination:
0138

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
AFAPL-TR-79-2064
Contract/Grant Number(s):
F33615-78-C-2060
Task Number(s):
15
Project Number(s):
3066
Monitor Series:
TR-79-2064
 Subject Terms
Joint Capability Areas:
JCA_5_Command and Control; JCA_5.3_Planning; JCA_5.3.4_Develop Courses of Action; JCA_5.3.5_Analyze Courses of Action; JCA_5.3.3_Develop Strategy; JCA_3.2_Engagement; JCA_3_Force Application; JCA_3.2.1_Kinetic Means; JCA_1.2_Force Preparation; JCA_1_Force Support; JCA_6_Net Centric; JCA_1.2.1_Training; JCA_6.1.3_Switching and Routing; JCA_4.3_Maintain
Communities of Interest:
No COI(s) Identified
Descriptor(s):
*TURBOFAN ENGINES, *EXPERIMENTAL DESIGN, *FANS, AERODYNAMIC CONFIGURATIONS, MATHEMATICAL MODELS, PARAMETERS, GRAPHS, FAN BLADES, AIRFOILS, BIRD STRIKES, REPLACEMENT, JET TRAINING AIRCRAFT, INGESTION(ENGINES), AERODYNAMICS
Field(s)/Group(s):
Training Aircraft, Jet and Gas Turbine Engines
Keyword(s):
High Bypass Turbofan Engines, WUAFAPL30661526, PE62203F
Report Date:
1979 Aug 01