Subsystem Design Analysis Lightweight Alternator (Model Test Program). Addendum 2.
Abstract
This report discusses the test and computer simulation activities conducted on a modified-design, small-rating aircraft alternator. These activities were intended to provide additional verifications of the alternator analytical approach utilized in designing two specialized large-rating lightweight alternators. The latter designs have been previously detailed in Air Force technical reports AFWL-TR-75-66, Subsystem Design Analysis Report for Lightweight Alternator (AC Load Case), and AFWL-TR-75-66, Addendum 1, Subsystem Design Analysis Report for Lightweight Alternator (DC Load Case). (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 01, 1977
- Accession Number
- ADA041257
Entities
People
- C. H. Lee
- D. Berker
- G. Tatro
- P. Walia