Component aerodynamic characteristics of banked cruciform missiles with arbitrary control deflections
- 8 August 1977
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Asymmetric Vortex Effects on Missile ConfigurationsJournal of Spacecraft and Rockets, 1975
- Static Aerodynamics of Missile Configurations for Mach O to 3Journal of Aircraft, 1975