A low-order potential-flow panel code, PMARC, for modeling complex three-dimensional geometries, is currently being developed at NASA Ames Research Center. The PMARC code was derived from a code named VSAERO that was developed for Ames Research Center by Analytical Methods, Inc. In addition to modeling potential flow over three-dimensional geometries, the present version of PMARC includes several advanced features such as an internal flow model, a simple jet wake model, and a time-stepping wake model. Data management within the code was optimized by the use of adjustable size arrays for rapidly changing the size capability of the code, reorganization of the output file and adopting a new plot file format. Preliminary versions of a geometry ...
© 1996, American Institute of Aeronautics and Astronautics, Inc. All Rights Reserved.The NASA-Ames d...
A low order panel method is described for the calculation of incompressible unsteady inviscid flow o...
An accurate and efficient method was developed for the aerodynamic analysis of a series of arbitrary...
The theoretical basis for PMARC, a low-order potential-flow panel code for modeling complex three-di...
The theoretical basis for PMARC, a low-order panel code for modeling complex three-dimensional bodie...
The CMARC panel code is evaluated to verify its accuracy and suitability for the development of an a...
A technique for determining wind tunnel wall effects for complex models using the low-order, three d...
The NASA-Ames developed panel code, PMARC, is employed to compute subsonic flows over an ogivecylind...
An evaluation of the ability of a low order panel method to predict complex three-dimensional intern...
The sizing and efficiency of an aircraft is largely determined by the performance of its high-lift s...
The National Aerospace Laboratories (NAL's) panel code capability buildup has been highlighted and s...
A subsonic, linearized aerodynamic theory, wing design program for one or two planforms was develope...
An examination of the potential flow computer code VSAERO to model leading edge separation over a de...
A two dimensional advanced panel far-field potential flow model of the undistorted, interacting wake...
The use of panel codes in the aerospace industry dates back many decades. Recent advances in compute...
© 1996, American Institute of Aeronautics and Astronautics, Inc. All Rights Reserved.The NASA-Ames d...
A low order panel method is described for the calculation of incompressible unsteady inviscid flow o...
An accurate and efficient method was developed for the aerodynamic analysis of a series of arbitrary...
The theoretical basis for PMARC, a low-order potential-flow panel code for modeling complex three-di...
The theoretical basis for PMARC, a low-order panel code for modeling complex three-dimensional bodie...
The CMARC panel code is evaluated to verify its accuracy and suitability for the development of an a...
A technique for determining wind tunnel wall effects for complex models using the low-order, three d...
The NASA-Ames developed panel code, PMARC, is employed to compute subsonic flows over an ogivecylind...
An evaluation of the ability of a low order panel method to predict complex three-dimensional intern...
The sizing and efficiency of an aircraft is largely determined by the performance of its high-lift s...
The National Aerospace Laboratories (NAL's) panel code capability buildup has been highlighted and s...
A subsonic, linearized aerodynamic theory, wing design program for one or two planforms was develope...
An examination of the potential flow computer code VSAERO to model leading edge separation over a de...
A two dimensional advanced panel far-field potential flow model of the undistorted, interacting wake...
The use of panel codes in the aerospace industry dates back many decades. Recent advances in compute...
© 1996, American Institute of Aeronautics and Astronautics, Inc. All Rights Reserved.The NASA-Ames d...
A low order panel method is described for the calculation of incompressible unsteady inviscid flow o...
An accurate and efficient method was developed for the aerodynamic analysis of a series of arbitrary...