Zobrazeno 1 - 10
of 37
pro vyhledávání: '"Vivek Mukhopadhyay"'
Publikováno v:
Environmental Impact of Aviation and Sustainable Solutions
Under the NASA Aeronautics Research Mission Directorate (ARMD) Convergent Aeronautical Solutions (CAS) project, NASA Glenn Research Center has been leading Multifunctional Structures for High Energy Lightweight Load-bearing Storage (M-SHELLS) researc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::20138f5b1fa15f7c83956631004d1908
http://www.intechopen.com/articles/show/title/structural-analysis-of-electric-flight-vehicles-for-application-of-multifunctional-energy-storage-sy
http://www.intechopen.com/articles/show/title/structural-analysis-of-electric-flight-vehicles-for-application-of-multifunctional-energy-storage-sy
Publikováno v:
AIAA Modeling and Simulation Technologies Conference.
NASA Environmentally Responsible Aviation (ERA) project and the Boeing Company are collabrating to advance the unitized damage arresting composite airframe technology with application to the Hybrid-Wing-Body (HWB) aircraft. The testing of a HWB fusel
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3ead468bda0cfba9877072d4c135ed9e
https://doi.org/10.2514/6.2015-3096
https://doi.org/10.2514/6.2015-3096
Publikováno v:
Journal of Aircraft. 41:925-930
Initial results of an investigation towards finding an efficient non-cylindrical fuselage configuration for a conceptual blended-wing-body flight vehicle were presented. A simplified 2-D beam column analysis and optimization was performed first. Then
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5116df2ebbf4246b6a4de417e60fc37d
https://doi.org/10.2514/1.417
https://doi.org/10.2514/1.417
Autor:
Vivek Mukhopadhyay
Publikováno v:
Journal of Guidance, Control, and Dynamics. 26:673-684
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c77e0c2cc7a66698aa7bcfe9c2c04708
https://doi.org/10.2514/2.5108
https://doi.org/10.2514/2.5108
Autor:
Vivek Mukhopadhyay
Publikováno v:
14th AIAA Aviation Technology, Integration, and Operations Conference.
Recent progress in the structural analysis of a Hybrid Wing-Body (HWB) fuselage concept is presented with the objective of structural weight reduction under a set of critical design loads. This pressurized efficient HWB fuselage design is presently b
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::151881026bbcd975693433382a30d2cf
https://doi.org/10.2514/6.2014-2427
https://doi.org/10.2514/6.2014-2427
Autor:
Vivek Mukhopadhyay
Publikováno v:
Journal of Guidance, Control, and Dynamics. 23:930-937
Fluttersuppressioncontrollawdesignandwind-tunneltestresultsintransonice owforaNACA0012wingmodel, under the benchmark active control technology program at NASA Langley Research Center, will be presented. Two control law design processes using classica
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ead82467a87b83036402c80ad080b37d
https://doi.org/10.2514/2.4635
https://doi.org/10.2514/2.4635
Autor:
Vivek Mukhopadhyay
Publikováno v:
Journal of Aircraft. 32:45-51
Design of a control law for simultaneously suppressing the symmetric and antisymmetric flutter modes of a sting-mounted, fixed-in-roll aeroelastic wind-tunnel model is described. The flutter suppression control law was designed using linear quadratic
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d34fc96d25c6696ebe7e67e19d119171
https://doi.org/10.2514/3.46682
https://doi.org/10.2514/3.46682
Autor:
Vivek Mukhopadhyay
Publikováno v:
53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference20th AIAA/ASME/AHS Adaptive Structures Conference14th AIAA.
This paper describes the interim progress for an in-house study that is directed toward innovative structural analysis and design of next-generation advanced aircraft concepts, such as the Hybrid Wing-Body (HWB) and the Advanced Mobility Concept-X fl
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8e0f08164ee2465a1749773120d2004b
https://doi.org/10.2514/6.2012-1999
https://doi.org/10.2514/6.2012-1999
Publikováno v:
Journal of Guidance, Control, and Dynamics. 15:878-884
A real-time controller, developed to implement flutter suppression and rolling maneuver load alleviation control laws digitally, was tested on an aeroelastic wind-tunnel model. A controller-per formance-evaluation (CPE) methodology to evaluate variou
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3e988707da31fe5db180e9490bff4b84
https://doi.org/10.2514/3.20920
https://doi.org/10.2514/3.20920