Accession Number:

ADA133399

Title:

A Study to Determine the Accuracy of Two Computer Programs in Predicting Hinge Moments for all Movable Tail Fins on Missile Bodies.

Descriptive Note:

Technical rept.,

Corporate Author:

ARMY MISSILE COMMAND REDSTONE ARSENAL AL SYSTEMS SIMULATION AND DEVELOPMENT DIRECTORATE

Personal Author(s):

Report Date:

1983-05-01

Pagination or Media Count:

28.0

Abstract:

The preliminary design of a guided missile with movable control surfaces requires an in-depth study of the aerodynamic loading experienced by these surfaces. Author.

Subject Categories:

  • Guided Missiles
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE