Techniques for Determining Missile Roll Parameters from a Wind Tunnel,
Abstract
A collection of the most prominent wind tunnel test techniques for determining missile aerodynamic roll parameters is presented. Both free-spin, and constrained-spin techniques are Presented along with each techniques' advantages and disadvantages. Special consideration is given to showing how the model bearing friction can be automatically cancelled from the roll balance measurement by an internal electric spin-motor. This technique alleviates the need for special bearing-friction tare measurements.
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 01, 1995
- Accession Number
- ADA307209
Entities
People
- Ronald T. Wincey
Organizations
- Defense Intelligence Agency