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) : Sanders,George A , III
PDF Url : ADA133399
Report Date : May 1983
Pagination or Media Count : 28
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).
Descriptors : *Guided missiles, *Aerodynamic control surfaces, *Aerodynamic loading, *Moments, *Fins, Computer programs, Accuracy, Predictions, Comparison, Slender bodies, Aspect ratio, Mach number, Coefficients, Angle of attack, Aerodynamic forces, Mathematical prediction, Taper, Tail assemblies
Subject Categories : Guided Missiles
Distribution Statement : APPROVED FOR PUBLIC RELEASE