Zobrazeno 1 - 10
of 47
pro vyhledávání: '"Jayanth N. Kudva"'
Autor:
Mark N. West, Jonathan D. Bartley-Cho, Jayanth N. Kudva, Christopher A. Martin, Donny P. Wang
Publikováno v:
Journal of Intelligent Material Systems and Structures. 15:279-291
The DARPA/AFRL/NASA Smart Wing program, led by Northrop Grumman Corporation (NGC) under the DARPA Smart Materials and Structures initiative, addressed the development of smart technologies and demonstration of relevant concepts to improve the aerodyn
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::acee03da6d319ef4a361eeef60b469a1
https://doi.org/10.1177/1045389x04042798
https://doi.org/10.1177/1045389x04042798
Autor:
Michael E. Pontecorvo, Robert Snyder, Ed V. White, Farhan Gandhi, Jayanth N. Kudva, Scott Bland, Silvestro Barbarino
Publikováno v:
55th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
This paper reports on the design, fabrication, testing and simulation of a novel structural element that combines load carrying and energy dissipation capability. The principal components comprise post-buckling elements (PBEs), and von-Mises trusses
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8d0dacf27eaff93f065e2ab0ebbb348a
https://doi.org/10.2514/6.2014-1203
https://doi.org/10.2514/6.2014-1203
Autor:
Ed V. White, Michael E. Pontecorvo, Scott Bland, Robert Snyder, Farhan Gandhi, Silvestro Barbarino, Jayanth N. Kudva
Publikováno v:
55th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
This paper presents a three-dimensional version of a planar hexagonal cell whose top and bottom inclined members act as a three-dimensional von-Mises truss (VMT), displaying negative stiffness or snap-through behavior. A damper connected between the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a6ee1b0887dd188cf34724ba5a6b06c3
https://doi.org/10.2514/6.2014-0501
https://doi.org/10.2514/6.2014-0501
Autor:
Jayanth N. Kudva, Harn C. Chen
Publikováno v:
International Journal of Fracture. 63:215-228
This paper presents a convenient and efficient method to obtain accurate stress intensity factors for cracked anisotropic plates. In this method, a complex variable formulation in conjunction with a hybrid displacement finite element scheme is used t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d70ae202d1f4951d28aafa1e34a70d30
https://doi.org/10.1007/bf00012469
https://doi.org/10.1007/bf00012469
Autor:
Shiv P. Joshi, Bryan Cannon, Jayanth N. Kudva, Jason Bowman, Brian Sanders, Terrence A. Weisshaar
Publikováno v:
48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e3aa840721a6f4d9e060416fb9111f59
https://doi.org/10.2514/6.2007-1730
https://doi.org/10.2514/6.2007-1730
Autor:
Jayanth N. Kudva, Akhilesh K. Jha
Publikováno v:
SPIE Proceedings.
A morphing aircraft can be defined as an aircraft that changes configuration to maximize its performance at radically different flight conditions. These configuration changes can take place in any part of the aircraft, e.g. fuselage, wing, engine, an
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7d9fcfc79d507c673fd9d11d70fa8e35
https://doi.org/10.1117/12.544212
https://doi.org/10.1117/12.544212
Autor:
Christopher A. Martin, Jayanth N. Kudva, Joseph A. Henderson, Northrop Grumman Integrated Systems
Publikováno v:
44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
Design of advanced aircraft structures requires information about the effects of constraints and performance parameters on the details of the optimized structure. Desire for radical increases in vehicle performance, fueled by advances in the field of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::12b253742ab7cceba322d03179c0430c
https://doi.org/10.2514/6.2003-1584
https://doi.org/10.2514/6.2003-1584
Publikováno v:
Smart Structures and Materials 2002: Industrial and Commercial Applications of Smart Structures Technologies.
The recently completed DARPA/AFRL/NASA Smart Wing program, performed by Northrop Grumman Corporation (NGC), addressed the development and demonstration of smart materials based concepts to improve the aerodynamic and aeroelastic performance of milita
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::65c523b28615891c1d242baaa7008d50
https://doi.org/10.1117/12.475083
https://doi.org/10.1117/12.475083
Publikováno v:
Smart Structures and Materials 2001: Smart Electronics and MEMS.
The proliferation of antenna systems of state-of-the-art military aircraft has challenged major airframe manufacturers to provide additional outer surface platform space for antenna placement while still maintaining a flightworthy structure. The solu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1d9ef1089e1fb3e97235b8ed89675247
https://doi.org/10.1117/12.436593
https://doi.org/10.1117/12.436593
Publikováno v:
SPIE Proceedings.
Over the last decade, Northrop Grumman Corporation under internal and DoD funding, and others, have been working on integration of RF antennas into load-bearing aircraft structures. This multidisciplinary effort, collectively referred to as Conformal
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5245dd98799134e5c916bd147604e61b
https://doi.org/10.1117/12.429688
https://doi.org/10.1117/12.429688