Zobrazeno 1 - 10
of 22
pro vyhledávání: '"Hampus Gavel"'
Publikováno v:
AIAA AVIATION 2021 FORUM.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6060feb08a3e35f146e84445d7fc4e10
https://doi.org/10.2514/6.2021-2998
https://doi.org/10.2514/6.2021-2998
Publikováno v:
Journal of Aerospace Information Systems. 13:219-233
An efficient methodology for verification, validation, and credibility assessment of simulation models and simulator applications is an enabler for the aeronautical industrys increasing reliance on ...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e67c076867523842980e4ddc74894111
https://doi.org/10.2514/1.i010391
https://doi.org/10.2514/1.i010391
Publikováno v:
Journal of Verification, Validation and Uncertainty Quantification. 2
Component-based system simulation models are used throughout all development phases for design and verification of both physical systems and control software, not least in the aeronautical industry. However, the application of structured methods for
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3b0199e636459bd189dff1f3bb61111d
https://doi.org/10.1115/1.4035716
https://doi.org/10.1115/1.4035716
Autor:
Hans Ellström, Hampus Gavel
Publikováno v:
Journal of Aircraft. 50:1038-1045
The prediction of the magnitude of the pressure surge in aircraft fuel systems is important from the standpoint of designing systems that will not exceed the maximum surge pressure allowed and also to determine the limit pressure so that lightweight
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a73979a44f5892c8d9ec67aae1957283
https://doi.org/10.2514/1.c031886
https://doi.org/10.2514/1.c031886
Publikováno v:
Computer-Aided Design. 41:187-196
This paper presents a formal mathematical framework for the use of the morphological matrix in a computerized conceptual design framework. Within the presented framework, the matrix is quantified so that each solution principle is associated with a s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cf0859c887fa14cb0bef9ed1890fe187
https://doi.org/10.1016/j.cad.2008.06.005
https://doi.org/10.1016/j.cad.2008.06.005
In a product development process, it is crucial to understand and evaluate multiple and synergic aspects of systems such as performance, cost, reliability, and safety. These aspects are mainly considered during later stages of the design process. How
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::dfd62ef504490bdec89c075e5846f6ca
http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-122539
http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-122539
The Environmental Control System (ECS) of the Saab Gripen fighter provides a number of vital functions, such as provision of coolant air to the avionics, comfort air to the cockpit, and pressurization of the aircraft fuel system. To support system de
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::78bb6df17db89e5deb7a55acbc97b99b
http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-142392
http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-142392
Publikováno v:
Journal of Aircraft. 43:1334-1340
This paper describes early considerations that have to be made when designing an aircraft fuel system. Emphasis is placed on illustrating the impact of top-level aircraft requirements on low-level practicalities such as fuel system design. Choosing b
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6951d415352dd55b41b6a4e4a029163d
https://doi.org/10.2514/1.19548
https://doi.org/10.2514/1.19548
Publikováno v:
Volume 4: Dynamics, Control and Uncertainty, Parts A and B.
To support early model validation, this paper describes a method utilizing information obtained from the common practice component level validation to assess uncertainties on model top level. Initiated in previous research, a generic output uncertain
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e8aaec26ff903c8090d1f2f6e268337b
https://doi.org/10.1115/imece2012-85236
https://doi.org/10.1115/imece2012-85236
Publikováno v:
AIAA Modeling and Simulation Technologies Conference.
Advances in recent years has brought forth many feasible technologies which oer signif-icant design advantages over the traditional aircraft vehicle ight systems. These advanceshave brought about a ...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1eeda10a848a1a37eb9f0b6a72eb15a4
https://doi.org/10.2514/6.2012-4716
https://doi.org/10.2514/6.2012-4716