Lamar M. Auman

发表

MissileLab User's Guide

Lamar M. Auman, Kristina Kirby-Brown, 2009 .

Recent Improvements to Missile DATCOM

Mark Underwood, Lamar M. Auman, Christopher Rosema, 2007 .

An Assessment of Productive Computational Fluid Dynamics for Aerodynamic Design

Lamar M. Auman, Milton E. Vaughn, 2008 .

Aerodynamic characteristics of a guided anti-tank missile utilizing a ram air powered control actuation system

Redstone Arsenal, Mark S. Miller, Lamar M. Auman, 1996 .

Assessment of a Productivity-Oriented CFD Methodology for Designing a Hypervelocity Missile

Lamar M. Auman, Milton E. Vaughn, 2003 .

An Initial Foray into the Productive Application of Computational Fluid Dynamics

Lamar M. Auman, Milton E. Vaughn, 2008 .

Recent Fin Related Improvements for Missile DATCOM

Redstone Arsenal, Mark Underwood, Lamar M. Auman, 2007 .

Recent Improvements for the 8/08 Release of Missile Datcom

Redstone Arsenal, Mark Underwood, Lamar M. Auman, 2009 .

Application of Fabric Ribbons for Drag and Stabilization

Redstone Arsenal, Lamar M. Auman, Brett L. Wilks, 2005 .

MISSILE DATCOM User's Manual - 2011 Revision

Mark Underwood, William B. Blake, Lamar M. Auman, 2008 .

A MATLAB/Aerodynamic Analyzer System Tool

Lamar M. Auman, Jonathan Newby, 2003 .

MissileLab: An Expert System for Aerodynamic Studies

Redstone Arsenal, Lamar M. Auman, Kristina Kirby-Brown, 2007 .

A PRODUCTIVITY-ORIENTED APPLICATION OF COMPUTATIONAL FLUID DYNAMICS TO THE DESIGN OF A HYPERVELOCITY MISSILE

Lamar M. Auman, Milton E. Vaughn, 2002 .

Aerodynamic Characteristics of a Canard-Controlled Missile with a Free-Spinning Tail

Missile Command, Richard E. Kreeger, Lamar M. Auman, 1998 .

Improvements in Fin-Shed Vortex Treatment for Missile Datcom

Redstone Arsenal, Lamar M. Auman, Christopher Rosema, 2009 .

Deflectable Nose and Canard Controls For a Fin -Stabilized Projectile At Supersonic and Hypersonic Speeds

Lamar M. Auman, Les Hall, Michael Landers, 2003 .