T-39 Landing Gear Design Evaluation and Fatigue Analysis. Phase II. Volume 1 of III,
Abstract
The purpose of this report is to accomplish a fatigue damage evaluation of the original and revised main and nose landing gears of the North American Rockwell T-39 aircraft. The fatigue loads spectrum utilized in this evaluation is developed by Bendix ECD from flight test data supplied by Hill Air Force Base.
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 28, 1975
- Accession Number
- ADA009878
Entities
People
- J. J. Wolfe
- W. W. Wagner