Unsteady Aerodynamic Vortex Lattice of Moving Aircraft
It is aim of this thesis to develop a potential ow solver for unsteady aerodynamics in MATLAB environment. In order to achieve this target a vortex lattice method based has been developed. The validation of this program involves two dierent stages. Initially, it is compared with classical experiment...
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| Format: | Others |
| Language: | English |
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KTH, Aerodynamik
2011
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-48928 |