HELICOPTER EXTERNAL SLING SYSTEM BASIC VIBRATION DATA.
Abstract
Simulated tests were conducted of helicopter externally slung loads ranging from 2,000 to 4,000 pounds on an analog computer. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 01, 1969
- Accession Number
- AD0699371
Entities
People
- George M. Cottingham