Fiscal Year	2008
Division	Graduate School of Engineering & Applied Science
Department	Mechanical & Aerospace Engineering
Investigator(s)	Chandrasekhara, Muguru S.
Sponsor	Defense Intelligence Agency (DoD)
Summary	The objective of this effort is to leverage the Naval Postgraduate School (NPS) knowledge and experience to develop efficient methods for six degree-of-freedom (6-DOF) missile aerodynamic coefficient estimation using emerging scientific concepts and the latest computational tools. The specific task is to develop a method and estimation aerodynamic coefficients for a generic SA-family missile with modified nose geometry.
Keywords	Missile Performance Prediction Approaches
Publications	Publications, theses (not shown) and data repositories will be added to the portal record when information is available in FAIRS and brought back to the portal
Data	Publications, theses (not shown) and data repositories will be added to the portal record when information is available in FAIRS and brought back to the portal