Combining experimental data, computational fluid dynamics, and six-degree of freedom simulation to develop a guidance actuator for a supersonic projectile
Author:
Affiliation:
1. Aerospace, Transportation, and Advanced Systems Laboratory, Georgia Tech Research Institute, Atlanta, Georgia, USA
2. Weapons and Materials Research Directorate, Army Research Laboratory, Aberdeen Proving Ground, Maryland, USA
Abstract
Publisher
SAGE Publications
Subject
Mechanical Engineering,Aerospace Engineering
Link
http://journals.sagepub.com/doi/pdf/10.1243/09544100JAERO399
Reference7 articles.
1. A Wall-Distance-Free k-ε Model With Enhanced Near-Wall Treatment
2. The Free Flight Aerodynamics Range
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