Zobrazeno 1 - 10
of 27
pro vyhledávání: '"David T. Chan"'
Autor:
Patrick R. Shea, David T. Chan, Morgan A. Walker, Sarah Langston, Jesse G. Collins, Lee Mears, Elizabeth Rieken, Jeremy Pinier
Publikováno v:
AIAA SCITECH 2023 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ca314dc487948348cc38113f2e70e72b
https://doi.org/10.2514/6.2023-0426
https://doi.org/10.2514/6.2023-0426
Autor:
John W. Paulson, David T. Chan, Kenneth G. Toro, Patrick R. Shea, Sean A. Commo, Peter A. Parker, Jeremy T. Pinier
Publikováno v:
AIAA Aviation 2019 Forum.
Low-speed wind tunnel testing for the liftoff and transition environment of the Space Launch System (SLS) was recently completed in the NASA Langley Research Center 14- by 22-Foot Subsonic Tunnel using 1.75%-scale models of three SLS vehicle configur
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e480ef7b325ace78f59297e465c62ff2
https://doi.org/10.2514/6.2019-3398
https://doi.org/10.2514/6.2019-3398
Autor:
Richard L. Campbell, Sally A. Viken, Scott L. Goodliff, Anthony Neal Watkins, Melissa B. Rivers, Michelle N. Lynde, David T. Chan
Publikováno v:
AIAA Scitech 2019 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cbe371d229c5835f6bc47322e11f47bb
https://doi.org/10.2514/6.2019-2189.c1
https://doi.org/10.2514/6.2019-2189.c1
Autor:
Peter A. Parker, Kenneth G. Toro, Sean A. Commo, David T. Chan, Patrick R. Shea, John W. Paulson
Publikováno v:
AIAA Scitech 2019 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f0a83596fa0516026c0dd1c444794ee4
https://doi.org/10.2514/6.2019-1839.c1
https://doi.org/10.2514/6.2019-1839.c1
Autor:
David T. Chan, John W. Paulson, Patrick R. Shea, Kenneth Toro, Peter A. Parker, Sean A. Commo
Publikováno v:
AIAA Scitech 2019 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e56b4f92ba23681f6e4c9660d09eae5b
https://doi.org/10.2514/6.2019-1839
https://doi.org/10.2514/6.2019-1839
Autor:
Melissa B. Rivers, Michelle N. Lynde, Richard L. Campbell, Sally A. Viken, David T. Chan, Anthony N. Watkins, Scott L. Goodliff
Publikováno v:
AIAA Scitech 2019 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3f3a8fda8542e370a43154f862847b7d
https://doi.org/10.2514/6.2019-2189
https://doi.org/10.2514/6.2019-2189
Autor:
Melissa B. Rivers, Richard L. Campbell, Anthony Neal Watkins, Michelle N. Lynde, Sally A. Viken, David T. Chan, Scott L. Goodliff
Publikováno v:
AIAA Scitech 2019 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::370c636245b05d79e5c2a39083997d44
https://doi.org/10.2514/6.2019-2298
https://doi.org/10.2514/6.2019-2298
Autor:
C. Mark Cagle, Scott L. Goodliff, William E. Milholen, Jared S. Fell, Gregory S. Jones, David T. Chan
Publikováno v:
2018 AIAA Aerospace Sciences Meeting.
The FAST-MAC circulation control model was modified to test an array of steady and unsteady actuators at realistic flight Reynolds numbers in the National Transonic Facility at the NASA Langley Research Center. Previous experiments in the FAST-MAC te
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::083d2a1d03dce8fecc14fcc9af023c80
https://doi.org/10.2514/6.2018-1138
https://doi.org/10.2514/6.2018-1138
Publikováno v:
Journal of Aircraft. 52:1736-1755
Recent wind-tunnel tests at the NASA Langley Research Center National Transonic Facility used high-pressure bellows to route air to the semispan model for evaluating aircraft circulation control testing techniques. The introduction of these bellows w
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8e9c7878e263134586589025f7e36d5d
https://doi.org/10.2514/1.c032942
https://doi.org/10.2514/1.c032942
Autor:
William E. Milholen, David T. Chan, Scott L. Goodliff, LaTunia G. Pack Melton, Gregory S. Jones, Christopher M. Cagle
Publikováno v:
35th AIAA Applied Aerodynamics Conference.
The FAST-MAC circulation control model was modified to test an array of unsteady sweeping-jet actuators at realistic flight Reynolds numbers in the National Transonic Facility at the NASA Langley Research Center. Two types of sweeping jet actuators w
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4f46c92f8b0f323caa5ceb32b218cb90
https://doi.org/10.2514/6.2017-3044
https://doi.org/10.2514/6.2017-3044