Zobrazeno 1 - 10
of 19
pro vyhledávání: '"Khanh V. Trinh"'
Autor:
Martynas Lendraitis, Christine Gregg, Joseph H. Kim, Greenfield Trinh, Kenneth C. Cheung, Sean Shan-Min Swei, Khanh V Trinh, Olivia Formoso, Benjamin Jenett, Nick B. Cramer, Daniel Cellucci
Publikováno v:
Smart Mater Struct
Ultralight materials present an opportunity to dramatically increase the efficiency of load-bearing aerostructures. To date, however, these ultralight materials have generally been confined to the laboratory bench-top, due to dimensional constraints
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d591583eb72bae5054734005be0bc74d
https://pubmed.ncbi.nlm.nih.gov/33479558
https://pubmed.ncbi.nlm.nih.gov/33479558
Autor:
Brian R. Taylor, Christine V. Jutte, John J. Burken, Khanh V. Trinh, Susan A. Frost, Marc Bodson
Publikováno v:
Journal of Aerospace Information Systems. 12:825-834
Advances in sensors and avionics computation power suggest real-time structural load measurements could be used in flight control systems for improved safety and performance. A conventional transport flight control system determines the moments neces
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::45e476fbef9625fb0e3dd65db4a91202
https://doi.org/10.2514/1.i010278
https://doi.org/10.2514/1.i010278
Publikováno v:
33rd AIAA Applied Aerodynamics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::742b9bf20adb57f9b58d51e0a5f26aca
https://doi.org/10.2514/6.2015-2723
https://doi.org/10.2514/6.2015-2723
Publikováno v:
32nd AIAA Applied Aerodynamics Conference.
This paper contains the development and optimization of an aeroelastic model of a flexible wing aircraft. The aircraft model is based on the NASA Generic Transport Model (GTM), with the wing structures of the model incorporating a novel aerodynamic c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::91f683a78af5406dfe67868f9c8b6c17
https://doi.org/10.2514/6.2014-2443
https://doi.org/10.2514/6.2014-2443
Publikováno v:
55th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
This paper presents a coupled vortex-lattice flight dynamic model with an aeroelastic finite-element model to predict dynamic characteristics of a flexible wing transport aircraft. The aircraft model is based on NASA Generic Transport Model (GTM) wit
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0540a2a5ab0e9d8ece09e8a58936e44e
https://doi.org/10.2514/6.2014-1040
https://doi.org/10.2514/6.2014-1040
Publikováno v:
55th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
This paper presents a static aeroelastic model and longitudinal trim model for the analysis of a flexible wing transport aircraft. The static aeroelastic model is built using a structural model based on finite-element modeling and coupled to an aerod
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2d1162c24ee0190a06d6a3120a437a24
https://doi.org/10.2514/6.2014-0837
https://doi.org/10.2514/6.2014-0837
Publikováno v:
55th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
This paper presents an aeroelastic method for predicting flutter characteristics of a flexible wing transport aircraft. The aircraft model is based on NASA Generic Transport Model (GTM) with representative mass and stiffness properties to achieve a w
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cc799602ac69ca323555f2cf832982c0
https://doi.org/10.2514/6.2014-0839
https://doi.org/10.2514/6.2014-0839
Publikováno v:
55th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
The emergence of advanced lightweight materials is resulting in a new generation of lighter, flexible, more-efficient airframes that are enabling concepts for active aeroelastic wing-shape control to achieve greater flight efficiency and increased sa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::510a00af682a669fbb862612875673e0
https://doi.org/10.2514/6.2014-1044
https://doi.org/10.2514/6.2014-1044
Publikováno v:
55th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
This paper presents an approach to the development of a scaled wind tunnel model for static aeroelastic similarity with a full-scale wing model. The full-scale aircraft model is based on the NASA Generic Transport Model (GTM) with flexible wing struc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::067813ec15255ae38643732e8159f624
https://doi.org/10.2514/6.2014-0838
https://doi.org/10.2514/6.2014-0838
Publikováno v:
AIAA Atmospheric Flight Mechanics (AFM) Conference.
This paper presents a coupled vortex-lattice flight dynamic model with an aeroelastic finite-element model to predict dynamic characteristics of a flexible wing transport aircraft. The aircraft model is based on NASA Generic Transport Model (GTM) wit
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b11271bf8191e6912cbd574e0187b1c3
https://doi.org/10.2514/6.2013-4746
https://doi.org/10.2514/6.2013-4746