METHODS AND SYSTEMS FOR ADAPTING A MULTI-BLOCK STRUCTURED MESH TOPOLOGY OF AN OBJECT TO A MODIFICATION IN ITS GEOMETRY
A computer-aided method for adapting a multi-block mesh topology of an object ( 11 ) to a modification in its geometry resulting from an operation defined in respect to some spatial directions, the method being used in the design of said object ( 11 ) by means of numerical simulation in structured meshes, comprising the following steps: a) providing the starting geometry ( 21 ) and mesh topology description ( 31 ); b) finding key points ( 25 ); c) finding the set of key vertexes placed at said key points ( 25 ); d) finding all the reference vertexes seeking for the vertexes connected to the key vertexes along said spatial directions; e) performing the geometrical operation and obtaining the adapted mesh topology moving said set of key vertexes to the position determined by the modified geometry ( 23 ) and the rest of vertexes proportionally to the displacement of the corresponding key vertex. The invention also refers to a system for carrying out said method.
1 . A computer-aided method for adapting a multi-block mesh topology of an object ( 11 ) to a modification in its geometry resulting from an operation defined in respect to one or more spatial directions, the method being used in the design of said object ( 11 ) by means of numerical simulation in entirely or partially structured meshes, characterised in that it comprises the following steps:
a) providing the starting geometry ( 21 ) of said object ( 11 ) and the starting mesh ( 31 ) topology description;
b) finding a set of key points ( 25 ) in the starting geometry ( 21 ) as the intersections of representative surfaces or curves ( 27 , 29 ) of said object ( 11 );
c) finding the set of key vertexes in the starting mesh ( 31 ) topology placed at said key points ( 25 );
d) finding all the reference vertexes involved in said operation seeking for the vertexes connected to said set of key vertexes along said one or more spatial directions;
e) performing said operation over the starting geometry ( 21 ) and obtaining the adapted mesh topology moving said set of key vertexes to the position determined by the modified geometry ( 23 ) and moving the rest of reference vertexes proportionally to the displacement of the corresponding key vertex.
2 . A method according to claim 1 , characterised in that step b) is carried out using a data base containing identification data of the key points for a set of standard geometry types.
3 . A method according to any of claim 1 , characterised in that said operation is one of the following: a translation, a rotation, a reprojection.
4 . A method according to claim 1 , characterised in that simulation tool is a CFD tool and said object ( 11 ) is an aircraft or a part of an aircraft.
5 . A system for adapting a multi-block structured mesh topology of an object ( 11 ) to a modification in its geometry resulting from an operation defined in respect to one or more directions, the system being used in the design of said object by means of numerical simulation in entirely or partially structured meshes, characterised in that it comprises:
a) A computer-implemented simulation model of said object ( 11 ).
b) Computer programs for carrying out at least in part the following operations:
b1) loading the starting geometry ( 21 ) of said object ( 11 ) and the starting mesh ( 31 ) topology description;
b2) finding a set of key points ( 25 ) in the starting geometry ( 21 ) as the intersections of representative surfaces or curves ( 27 , 29 ) of said object ( 11 );
b3) finding the set of key vertexes in the starting mesh ( 31 ) topology placed at said key points ( 25 );
b4) finding all the reference vertexes involved in said operation seeking for the vertexes connected to said set of key vertexes along said one or more spatial directions;
b5) performing said operation over the starting geometry ( 21 ) and obtaining the adapted mesh topology moving said set of key vertexes to the position determined by the modified geometry ( 23 ) and moving the rest of reference vertexes proportionally to the displacement of the corresponding key vertex.
6 . A system according to claim 5 , characterised in that it also comprises a data base containing identification data of the key points for a set of standard geometry types.
7 . A method according to claim 5 , characterised in that said operation is one of the following: a translation, a rotation, a reprojection.
8 . A method according to claim 5 , characterised in that said simulation model is a CFD model and said object ( 11 ) is an aircraft or a part of an aircraft.