Accession Number:

ADB010051

Title:

Advanced Aerodynamic Control Technology

Descriptive Note:

Summary rept. Jul 1973-Jun 1975

Corporate Author:

NAVAL WEAPONS CENTER CHINA LAKE CA

Personal Author(s):

Report Date:

1976-01-08

Pagination or Media Count:

40.0

Abstract:

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.

Subject Categories:

  • Guided Missile Dynamics, Configurations and Control Surfaces

Distribution Statement:

APPROVED FOR PUBLIC RELEASE