SECURITY CLASSIFICATION OF ABSTRACT Unclassified 20. SECURITY CLASSIFICATION OF THIS PAGE Unclassified 19. SECURITY CLASSIFICATION OF REPORT Unclassified 18. SUBJECT TERMS ANSYS, CFX, canard, Computational Fluid Dynamics, missile, AP NUMBER OF PAGES PRICE CODE 17. The AP09 results also showed good agreement for C N, C M, and C L but also showed less agreement for C A. The ANSYS-CFX results showed good agreement for C N, C M, and C L but less agreement for C A when compared to the experimental results. The results were compared against experimental data from actual wind tunnel tests and data from a semi-empirical method, AP09. The study was conducted for Mach numbers of 0.2, 0.8 and 1.2. DISTRIBUTION CODE This study used the Computational Fluid Dynamics code, ANSYS-CFX to predict the static aerodynamic characteristics of a canard-wing missile configuration with a hemispherical nose, triangular wedge canards and fixed trapezoidal wings. DISTRIBUTION / AVAILABILITY STATEMENT Approved for public release distribution is unlimited 13. SUPPLEMENTARY NOTES The views expressed in this thesis are those of the author and do not reflect the official policy or position of the Department of Defense or the U.S. SPONSORING/MONITORING AGENCY REPORT NUMBER 11. PERFORMING ORGANIZATION REPORT NUMBER 10. PERFORMING ORGANIZATION NAME(S) AND ADDRESS(ES) Naval Postgraduate School Monterey, CA SPONSORING /MONITORING AGENCY NAME(S) AND ADDRESS(ES) N/A 8.
FUNDING NUMBERS Configuration using ANSYS-CFX 6. TITLE AND SUBTITLE Aerodynamic Analysis of a Canard Missile 5. REPORT DATE December REPORT TYPE AND DATES COVERED Master s Thesis 4. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden, to Washington headquarters Services, Directorate for Information Operations and Reports, 1215 Jefferson Davis Highway, Suite 1204, Arlington, VA, and to the Office of Management and Budget, Paperwork Reduction Project ( ) Washington DC AGENCY USE ONLY (Leave blank) 2. 2 NAVAL POSTGRADUATE SCHOOL MONTEREY, CALIFORNIA THESIS AERODYNAMIC ANALYSIS OF A CANARD MISSILE CONFIGURATION USING ANSYS-CFX by Hong Chuan Wee Thesis Advisor: Second Reader: December 2011 Maximilian Platzer Garth Hobson Approved for public release distribution is unlimitedĤ REPORT DOCUMENTATION PAGE Form Approved OMB No Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instruction, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information.
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