Zobrazeno 1 - 10
of 11
pro vyhledávání: '"Jared C. Duensing"'
Autor:
Emre Sozer, Jeffrey A. Housman, Michael G. Piotrowski, Gaetan K. W. Kenway, Cetin C. Kiris, Jared C. Duensing, James C. Jensen, Daniel Maldonado
Publikováno v:
Journal of Aircraft. 59:624-646
Predictions using the launch ascent and vehicle aerodynamics (LAVA) solver framework for the NASA shock–plume interaction biconvex model and C608 supersonic aircraft prototype geometries are compar...
Publikováno v:
AIAA SCITECH 2023 Forum.
Publikováno v:
AIAA AVIATION 2022 Forum.
Publikováno v:
AIAA SCITECH 2022 Forum.
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.
High-Lift Common Research Model: RANS, HRLES, and WMLES perspectives for CLmax prediction using LAVA
Autor:
Cetin C. Kiris, Aditya S. Ghate, Jared C. Duensing, Oliver M. Browne, Jeffrey A. Housman, Gerrit-Daniel Stich, Gaetan Kenway, Luis M. Dos Santos Fernandes, Leonardo M. Machado
Publikováno v:
AIAA SCITECH 2022 Forum.
Publikováno v:
AIAA SCITECH 2022 Forum.
Autor:
Jeffrey A. Housman, Michael G. Piotrowski, Jared C. Duensing, Emre Sozer, Daniel Maldonado, Cetin C. Kiris, Gaetan K. Kenway, James C. Jensen
Publikováno v:
AIAA Scitech 2021 Forum.
Autor:
Daniel Maldonado, Craig A. Hunter, Sally A. Viken, Jared C. Duensing, S. Naomi McMillin, Neal T. Frink, Jeffrey A. Housman, James C. Jensen, Cetin C. Kiris
Publikováno v:
AIAA Scitech 2020 Forum.
A joint effort between the NASA Ames and Langley Research Centers was undertaken to analyze the Mach 0.745 variant of the Boeing Transonic Truss-Braced Wing (TTBW) Design. Two different flow solvers, LAVA and USM3D, were used to predict the TTBW flig
Autor:
Jared C. Duensing, Seung Y. Yoo
Publikováno v:
AIAA Aviation 2019 Forum.
Investigations of the external aerodynamics of the unpowered X-57 Mod-III configuration using computational fluid dynamics are presented. Two different Reynolds-averaged Navier-Stokes flow solvers were used in the analysis: the STAR-CCM+ unstructured