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pro vyhledávání: '"Munjulury, Raghu Chaitanya"'
Autor:
Munjulury, Raghu Chaitanya
The design and development of new aircraft are becoming increasingly expensive and timeconsuming. To assist the design process in reducing the development cost, time, and late design changes, the conceptual design needs enhancement using new tools an
Externí odkaz:
http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-137646
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2018, Vol. 90, Issue 7, pp. 1128-1135.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-01-2017-0046
Akademický článek
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Autor:
Munjulury, Raghu Chaitanya, Nadali Najafabadi, Hossein, Safavi, Edris, Ölvander, Johan, Petter, Krus, Karlsson, Matts
Publikováno v:
Advances in Mechanical Engineering, Vol 9 (2017)
Multidisciplinary design optimization has become a powerful technique to facilitate continuous improvement of complex and multidisciplinary products. Parametric modeling is an essential part with tremendous impact on the flexibility and robustness of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::4c32927be7b00332a338cdd5be1eb04d
http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-137645
http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-137645
The architecture of the flight control system, essentialfor all flight operations, has significantlychanged throughout the years. The first part ofthe work consists of a preliminary sizing modelof an EHA and an EMA. The second part of thework consist
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::560112612d6b0a0e4cd76b3a5bcf4d43
http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-120619
http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-120619
Landing gear weight calculations can be carried out using statistical or analytical methods. Statistical methods were used in the past and offered quick group weights, however, they are not capable of computing with accuracy the weight of unconventio
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::2ba905f642e3d72caf02642568f547cd
http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-119125
http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-119125
This work presents knowledge-based parametricdefinition of aircraft fuel systems, oriented to itsuse in conceptual design and integrated into theRAPID design tool. Fuel systems appear earlyin the design process as they are involved in severalfirst es
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::2f1af7ad7cf07190137c9e7f2a03b787
http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-120572
http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-120572
Akademický článek
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Publikováno v:
IOP Conference Series: Materials Science and Engineering; February 2022, Vol. 1226 Issue: 1 p012111-012111, 1p