Zobrazeno 1 - 10
of 12
pro vyhledávání: '"Brett R. Hiller"'
Publikováno v:
AIAA SCITECH 2022 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d5f63b35701c81d134466d47ff26c207
https://doi.org/10.2514/6.2022-1680
https://doi.org/10.2514/6.2022-1680
Autor:
Ralph Jansen, Cetin C. Kiris, Timothy Chau, Leonardo M. Machado, Jared C. Duensing, Arman Mirhashemi, Jeffryes Chapman, Brad D. French, Lilia Miller, Jonathan S. Litt, Casey L. Denham, Michelle N. Lynde, Richard L. Campbell, Brett R. Hiller, Nathaniel J. Blaesser, Nic Heersema
Publikováno v:
AIAA SCITECH 2022 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::51bed22f549dda8b25380e941dbcd5c0
https://doi.org/10.2514/6.2022-2179
https://doi.org/10.2514/6.2022-2179
Publikováno v:
AIAA SCITECH 2022 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::39356c1b66975e7b46aaf46c535bed61
https://doi.org/10.2514/6.2022-2303
https://doi.org/10.2514/6.2022-2303
Publikováno v:
AIAA AVIATION 2021 FORUM.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8b1672ca75488da294433ac1680a0f77
https://doi.org/10.2514/6.2021-2525
https://doi.org/10.2514/6.2021-2525
Publikováno v:
AIAA Scitech 2021 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::609068ec2b05131d2a5de1d4296bf492
https://doi.org/10.2514/6.2021-0173
https://doi.org/10.2514/6.2021-0173
Publikováno v:
AIAA Aviation 2019 Forum.
A reduced-order modeling method capable of providing computationally efficient predictions of the nonlinear, unsteady aerodynamics encountered by flexible flight vehicles under- going forced oscillations is presented. Models are developed using indic
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1df9f0407721405ea893eb4c388efbba
https://doi.org/10.2514/6.2019-3388
https://doi.org/10.2514/6.2019-3388
Publikováno v:
AIAA Scitech 2019 Forum.
High-fidelity computational fluid dynamics tools offer the potential to approximate increments for ground-to-flight scaling effects, as well as to augment the dynamic damping derivative data for motion-based flight simulators. Unfortunately, the comp
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f0269bd32559fb2d229bfd912c7617db
https://doi.org/10.2514/6.2019-0980
https://doi.org/10.2514/6.2019-0980
Publikováno v:
2018 Applied Aerodynamics Conference.
Within the NATO STO AVT-251 Task Group, a generic Unmanned Combat Air Vehicle (UCAV) planform was redesigned based on requirements derived from parts of the flight envelope of the defined mission. Because of the lambda-shape planform and associated f
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2ea08807fb5b7a240ca32248e354e410
https://doi.org/10.2514/6.2018-2998
https://doi.org/10.2514/6.2018-2998
Publikováno v:
2018 AIAA Atmospheric Flight Mechanics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1440b6be53714153d9706c53b7321bdc
https://doi.org/10.2514/6.2018-0291
https://doi.org/10.2514/6.2018-0291
Publikováno v:
2018 AIAA Atmospheric Flight Mechanics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0dd2cf3512144bc846f7c5f973132b21
https://doi.org/10.2514/6.2018-0292
https://doi.org/10.2514/6.2018-0292