This report documents the computer program developed by the Army to evaluate and implement an aerodynamic methodology developed by the Martin Marietta Corporation. The methodology was developed to predict aerodynamic forces on slender missile bodies with low aspect ratio tails at low and high angles of attack, at arbitrary roll angles for both transonic and supersonic velocities. (Author)
User's Manual for the Martin-Marietta High Angle of Attack Aerodynamic Methodology for Body Tail Missiles
1978
81 pages
Report
No indication
English
Missile Trajectories & Reentry Dynamics , Missile Technology , Aerodynamic forces , Slender bodies , Computer program documentation , Tail assemblies , Aerodynamic configurations , Computer programs , Aerodynamic characteristics , Mathematical prediction , Angle of attack , Aspect ratio , Roll , Transonic flow , Supersonic flow , Subroutines , Guided missiles
Elsevier | 1986
Martin Marietta goes for growth
Online Contents | 1993
|Martin Marietta splits off visuals
Online Contents | 1994