EFFECT OF DYNAMIC IMBALANCE ON THE MOTION OF A SPINNING VEHICLE IN FREE FLIGHT,
Abstract
The principal moments of inertia and the location of the principal axes of a slightly asymmetrical body are determined. The Euler equations for a freely rotating body are solved approximately, assuming that the body is almost symmetric. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 30, 1962
- Accession Number
- AD0608678
Entities
People
- J. S. Holmstrom
Organizations
- Stellantis North America (formerly Chrysler)