A development status evaluation is presented for the aerodynamics of missile configurations with noncircular cross-sections and bank-to-turn maneuvering systems, giving attention to cases with elliptical and square cross-sections, as well as bodies with variable cross-sections. The assessment of bank-to-turn missile performance notes inherent stability/control problems. A summary and index are provided for aerodynamic data on monoplanar configurations, including those which incorporate airbreathing propulsion systems.
Bodies with noncircular cross sections and bank-to-turn missiles
1992-01-01
Miscellaneous
No indication
English
Wing-Body Carryover for Noncircular Missiles
Online Contents | 1995
|Investigation of Bank-to-Turn Missiles
NTIS | 1986
|Wing-body carryover for noncircular missiles
AIAA | 1995
|