Studying aeroelastic behavior of aircraft with NeoCASS.: The Danbus configuration
Independent thesis Advanced level (degree of Master (One Year)), 20 credits / 30 HE creditsStudent thesis
This Master Thesis assesses the performance of NeoCASS software as a tool for structural sizing for deformable aircraft at conceptual design level. NeoCASS is a collection of Matlab modules included in CEASIOM. Some testcases (simple wing model, TCR, Danbus, Agard 445.6 wing) are computed to evaluate the aeroelastic behavior and provide additional validation on the structural models NeoCASS computes Finally, Danbus, a new conceptual design aircraft, is analyzed with the software.
Place, publisher, year, edition, pages
2011. , 85 p.
Trita-AVE, ISSN 1651-7660 ; 2011:43
Engineering and Technology
IdentifiersURN: urn:nbn:se:kth:diva-39370OAI: oai:DiVA.org:kth-39370DiVA: diva2:439828
Subject / course
Master of Science in Engineering - Vehicle Engineering
Rizzi, Arthur, Prof