Comparison of Aerodynamic Methods for the Computation of Control Surface Loads
This paper presents loads computations for the generic UCAV configuration F19, originally devised by the German Aerospace Center (DLR). Different aerodynamic methods are investigated and their effect on concentrated structural loads is assessed. Design manoeuvres are defined based on the manoeuvre a...
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| Format: | Others |
| Language: | English |
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KTH, Flygdynamik
2015
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-185022 |