Accession Number : ADA333445
Title : Evaluation of the CMARC Panel Code Software Suite for the Development of a UAV Aerodynamic Model
Descriptive Note : Master's thesis
Corporate Author : NAVAL POSTGRADUATE SCHOOL MONTEREY CA
Personal Author(s) : Pollard, Stephen J.
PDF Url : ADA333445
Report Date : JUN 1997
Pagination or Media Count : 151
Abstract : The CMARC panel code is evaluated to verify its accuracy and suitability for the development of an aerodynamic model of the Naval Postgraduate School (NPS) FROG Unmanned Air Vehicle (UAV). CMARC is a DOS personal computer based version of the NASA Panel Method Ames Research Center (PMARC) panel code. The core processing algorithms in CMARC are equivalent to PMARC. CMARC enhancements include improved memory management and command line functionality. Both panel codes solve for inviscid, incompressible flow over complex three-dimensional bodies using potential flow theory. Emphasis is first placed on verifying CMARC against the PMARC and NPS Unsteady Potential Flow (UPOT) panel codes. CMARC boundary layer calculations are then compared to experimental data for an inclined prolate spheroid. Finally, a complex three-dimensional panel model is developed for aerodynamic modeling of the FROG UAV. CMARC off-body flow field calculations are used to generate static-source and angle-of-attack vane position corrections. Position corrections are provided in look-up table and curve fit formats. Basic longitudinal and lateral-directional stability derivatives are also developed with CMARC data. CMARC derived stability derivatives are sufficiently accurate for incorporation into an initial aerodynamic model. Adjustments through analysis of flight test data may be required. Future CMARC studies should concentrate on the development of the damping and control power derivatives.
Descriptors : *COMPUTATIONAL FLUID DYNAMICS, *COMPUTER PROGRAM VERIFICATION, *AERODYNAMICS, SOFTWARE ENGINEERING, AERODYNAMIC STABILITY, THESES, BOUNDARY LAYER, FLOW FIELDS, HYDRODYNAMIC CODES, AIRCRAFT MODELS, INVISCID FLOW, REMOTELY PILOTED VEHICLES, INCOMPRESSIBLE FLOW, POTENTIAL FLOW, THREE DIMENSIONAL FLOW.
Subject Categories : Aerodynamics
Computer Programming and Software
Distribution Statement : APPROVED FOR PUBLIC RELEASE