SIMULATION STUDY OF PROPOSED YAW DAMPER SYSTEMS FOR THE B-58 AIRCRAFT
Abstract
Computer analysis of yaw damper systems proposed for modification of the B-58 Aircraft. Results generally verified conclusions and recommendations of contractor studies with the exception of low speed characteristics. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1966
- Accession Number
- AD0804085
Entities
People
- Raymond L. Haas
Organizations
- Flight Dynamics Laboratory