Zobrazeno 1 - 10
of 40
pro vyhledávání: '"S, Winski"'
Autor:
J. Fischer, K. Bouhana, M.J. Chicarelli, J. Dahlke, B. Fell, J. Fulton, A. Guarnieri, L. Haygood, R. Jalluri, A. Johnson, B. McLean, M. Max, R. Rieger, J. Robinson, M. Rodriguez, F. Sullivan, Y. Wang, S. Winski, Y. Zhou
Publikováno v:
European Journal of Cancer. 174:S81
Autor:
M.J. Chicarelli, K. Bouhana, L. Cable, M. Crow, B. Fell, J. Fischer, J. Fulton, A. Guarnieri, R. Jalluri, J. Robinson, F. Sullivan, S. Winski, Y. Zhou
Publikováno v:
European Journal of Cancer. 174:S81
Autor:
Andre Ribeiro, Patrick R. Shea, Mehdi R. Khorrami, Courtney S. Winski, Ryan Ferris, Michael Sacks, Patricio A. Ravetta
Publikováno v:
AIAA AVIATION 2021 FORUM.
Autor:
Jeremy T. Pinier, Paul M. Danehy, A. Neal Watkins, Heather P. Houlden, Jamie G. Meeroff, Courtney S. Winski, Patrick R. Shea, K. Todd Lowe
Publikováno v:
AIAA Aviation 2019 Forum.
A wind tunnel test was run in the NASA Langley Unitary Plan Wind Tunnel simulating the separation of the two solid rocket boosters (SRB) from the core stage of the NASA Space Launch System (SLS). The test was run on a 0.9% scale model of the SLS Bloc
Publikováno v:
AIAA Scitech 2019 Forum.
Autor:
Paul M. Danehy, Kevin T. Lowe, Courtney S. Winski, Jamie G. Meeroff, Anthony Neal Watkins, Patrick R. Shea, Heather P. Houlden
Publikováno v:
AIAA Scitech 2019 Forum.
Autor:
Courtney S. Winski, Paul M. Danehy, Anthony N. Watkins, Patrick R. Shea, Jamie G. Meeroff, Kevin T. Lowe, Heather P. Houlden
Publikováno v:
AIAA Scitech 2019 Forum.
Autor:
Matthew T. Boyda, Bryan E. Falman, Kevin T. Lowe, Sean Shea, Bradley M. Wisser, Timothy W. Fahringer, Courtney S. Winski, Paul M. Danehy
Publikováno v:
AIAA Scitech 2019 Forum.
Planar flow visualizations were obtained in a wind tunnel test in the NASA Langley Research Center’s Unitary Plan Wind Tunnel using the laser-light-sheet method. This method uses a laser to illuminate fine particles generated in the wind tunnel to
Publikováno v:
AIAA Scitech 2019 Forum.
Autor:
Courtney S. Winski, Sudheer N. Nayani, Melissa B. Carter, Jason M. Pearl, Alaa Elmiligui, Donald A. Durston
Publikováno v:
2018 AIAA Aerospace Sciences Meeting.
A wind tunnel test was performed in the NASA Ames 9x7 Supersonic Wind Tunnel focusing on the shock waves traveling through and interacting with an exhaust nozzle plume. This experimental study was conducted to develop and validate the CFD capability