Accession Number : ADA354951


Title :   Development and Verification of an Aerodynamic Model for the NPS Frog UAV Using the CMARC Panel Code Software Suite


Descriptive Note : Thesis,


Corporate Author : NAVAL POSTGRADUATE SCHOOL MONTEREY CA


Personal Author(s) : Pollard, Stephen J.


Full Text : http://www.dtic.mil/get-tr-doc/pdf?AD=ADA354951


Report Date : SEP 1998


Pagination or Media Count : 195


Abstract : The CMARC panel-code is evaluated for the development of an aerodynamic model of the Naval Postgraduate School FROG Unmanned Air Vehicle (UAV). CMARC is a personal computer hosted panel-code software suite for solving inviscid, incompressible flow over complex three-dimensional bodies. A panel model of the NPS FROG UAV is developed to obtain stability derivative data at the cruise flight condition. Emphasis is placed on comparing the CMARC data to aerodynamic models obtained from classical design techniques and parameter estimation. Linearized longitudinal and lateral-directional state-equation models are used to compare the dynamic response of each data set. In addition, CMARC is used to generate static-source and angle-of-attack sensor position corrections. Position corrections are provided in look-up table and curve-fit formats. The aerodynamic model obtained with CMARC demonstrated higher fidelity dynamic longitudinal response than the classical design model. Dynamic lateral-directional response is similar to that obtained from classical design techniques. Adjustment through comparison with flight-test data is still required to optimize the CMARC model. Future studies should concentrate on improving CMARC modeling of fuselage side force through the addition of wake separation lines. Additionally, the propeller disk should be modeled in an attempt to capture the effects of increased dynamic pressure over the horizontal and vertical tail surfaces.


Descriptors :   *AERODYNAMIC CHARACTERISTICS , *REMOTELY PILOTED VEHICLES , COMPUTER PROGRAMS , DATA BASES , FLIGHT TESTING , STABILITY , DETECTORS , FLIGHT CONTROL SYSTEMS , VERIFICATION , PARAMETERS , TAIL ASSEMBLIES , DYNAMIC RESPONSE , THESES , ANGLE OF ATTACK , ESTIMATES , SURFACES , CODING , FLIGHT , VERTICAL ORIENTATION , AERODYNAMIC LOADING , FUSELAGES , TABLES(DATA) , MICROCOMPUTERS , DYNAMIC PRESSURE , CORRECTIONS , HORIZONTAL STABILIZERS , AERIAL PROPELLERS.


Subject Categories : AERODYNAMICS
      PILOTLESS AIRCRAFT
      COMPUTER PROGRAMMING AND SOFTWARE


Distribution Statement : APPROVED FOR PUBLIC RELEASE