DRAG AND STABILITY COEFFICIENTS FOR FOUR SPHERICAL-TIPPED OGIVAL NOSES FROM M=1.53 TO M=4.99.
Abstract
The results of wind tunnel tests made on four spherical-tipped ogival noses at M=1.53 to 4.99 are presented. Normal force, pitching moment, axial force, and base pressure coefficients were obtained for an angle of attack range of + or - 5 degrees. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 01, 1967
- Accession Number
- AD0380168
Entities
People
- John A. Darling
Organizations
- Naval Ordnance Laboratory