| dc.creator |
Tan, Bui-Thanh |
|
| dc.creator |
Willcox, Karen E. |
|
| dc.creator |
Damodaran, Murali |
|
| dc.date |
2003-11-17T17:08:20Z |
|
| dc.date |
2003-11-17T17:08:20Z |
|
| dc.date |
2003-01 |
|
| dc.date.accessioned |
2013-10-09T02:32:03Z |
|
| dc.date.available |
2013-10-09T02:32:03Z |
|
| dc.date.issued |
2013-10-09 |
|
| dc.identifier |
http://hdl.handle.net/1721.1/3694 |
|
| dc.identifier.uri |
http://koha.mediu.edu.my:8181/xmlui/handle/1721 |
|
| dc.description |
Two extensions to the proper orthogonal decomposition (POD) technique are considered for steady transonic aerodynamic applications. The first is to couple the POD approach with a cubic spline interpolation procedure in order to develop fast, low-order models that accurately capture the variation in parameters, such as the angle of attack or inflow Mach number. The second extension is a POD technique for the reconstruction of incomplete or inaccurate aerodynamic data. First, missing flow field data is constructed with an existing POD basis constructed from complete aerodynamic data. Second, a technique is used to develop a complete snapshots from an incomplete set of aerodynamic snapshots. |
|
| dc.description |
Singapore-MIT Alliance (SMA) |
|
| dc.format |
1620170 bytes |
|
| dc.format |
application/pdf |
|
| dc.language |
en_US |
|
| dc.relation |
High Performance Computation for Engineered Systems (HPCES); |
|
| dc.subject |
Proper Orthogonal Decomposition |
|
| dc.subject |
inviscid transonic aerodynamics |
|
| dc.subject |
flow fields |
|
| dc.subject |
cubic spline interpolation procedure |
|
| dc.title |
Applications of Proper Orthogonal Decomposition for Inviscid Transonic Aerodynamics |
|
| dc.type |
Article |
|