Advanced Aerodynamic Control Technology
Summary rept. Jul 1973-Jun 1975
NAVAL WEAPONS CENTER CHINA LAKE CA
Pagination or Media Count:
The objective of the work described in this report was to develop a better understanding of the aerodynamic roll characteristics of canard controlled missiles. Studies were performed to develop a method of predicting induced roll moments, a method for simplified representation of aerodynamic coefficients in simulations, and to evaluate the use of canard and tail slots.
- Guided Missile Dynamics, Configurations and Control Surfaces