Static-Stability and Roll-Damping Coefficients for a Slender Blunted Cone Showing the Effects of Spin, Angle of Attack, and Center-of-Gravity Offset AT M=5 and 7.7,
Abstract
Results are presented from wind-tunnel tests performed in a hypersonic tunnel at M = 4.96, 5.01 and 7.70. During these tests normal-force, pitching-moment and roll-damping coefficients were obtained on a 7.25-degree, 0.075 bluntness cone model, for a pd/2V (average roll parameter) value of 0.02 to show the effect of spin, angle of attack, and center-of-gravity offset. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 10, 1969
- Accession Number
- AD0863650
Entities
People
- John A. Darling
Organizations
- Naval Ordnance Laboratory