Accession Number:

AD1094343

Title:

Control Surface Design Analysis for Munitions

Descriptive Note:

Technical Report,01 Jun 2019,01 Nov 2019

Corporate Author:

U.S. Army Combat Capabilities Development Command Army Research Laboratory Aberdeen Proving Ground United States

Report Date:

2020-03-01

Pagination or Media Count:

24.0

Abstract:

Enhancing munition maneuverability is a key enabling technology for both range extension and terminal maneuvers of long-range precision munitions. One approach to munition maneuverability is to deflect control surfaces to achieve body attack angles that generate lift from the body and other aerodynamic surfaces. This report presents a methodology to analyze aerodynamic control surfaces to determine effectiveness at generating a pitching or yawing moment on a projectile to attain an angle of attack that produces significant lateral accelerations in flight. The methodology demonstrated in this report is for a gun-launched, aerodynamically stabilized, fin-controlled projectile, but is applicable to other control surface design problems.

Subject Categories:

  • Guided Munitions
  • Aerodynamics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE