Zobrazeno 1 - 10
of 28
pro vyhledávání: '"John W. Paulson"'
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:
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
Publikováno v:
Journal of Spacecraft and Rockets. 49:564-573
An investigation has been conducted in the NASA Langley Research Center 14- by 22Foot Subsonic Wind Tunnel to obtain the liftoff and transition aerodynamics of the Ares I (A106) Crew Launch Vehicle. Data were obtained in free-air at angles of attack
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::75cc7dea382d2ab814d7b9ed5d69622f
https://doi.org/10.2514/1.a32198
https://doi.org/10.2514/1.a32198
Autor:
Gary E. Erickson, John Blevins, William G. Tomek, Jeremy T. Pinier, David W. Bennett, John W. Paulson
Publikováno v:
53rd AIAA Aerospace Sciences Meeting.
A 1.75% scale force and moment model of the Space Launch System was tested in the NASA Langley Research Center 14- by 22-Foot Subsonic Wind Tunnel to quantify the aerodynamic forces that will be experienced by the launch vehicle during its liftoff an
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7087061ace58bcd37cd7054279b275b4
https://doi.org/10.2514/6.2015-0775
https://doi.org/10.2514/6.2015-0775
Publikováno v:
Journal of Spacecraft and Rockets. 32:758-764
During the high-Mach-number, high-altitude portion of the first entry of the Shuttle Orbiter, the vehicle exhibited a nose-up pitching moment relative to preflight prediction of approximately Delta Cm = 0.03. This trim anomaly has been postulated to
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5636d2e82c6ef6cecd27a186119aaeca
https://doi.org/10.2514/3.26680
https://doi.org/10.2514/3.26680
Publikováno v:
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
An investigation has been conducted in the NASA Langley Research Center 14- by 22- Foot Subsonic Wind Tunnel to obtain the liftoff and transition aerodynamics of the Ares I (A106) Crew Launch Vehicle. Data were obtained in free-air at angles of attac
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1c61a89a3eb54d3dc85f8a5b215cb92a
https://doi.org/10.2514/6.2011-997
https://doi.org/10.2514/6.2011-997
Publikováno v:
32nd Aerospace Sciences Meeting and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a30016c229c7181b1757192dc56b0bfc
https://doi.org/10.2514/6.1994-632
https://doi.org/10.2514/6.1994-632
Publikováno v:
The Journal of the Acoustical Society of America. 99:1282
A system for interpreting the requests and performance of an instrumental soloist, stated in the parlance of the musician and within the context of a specific published edition of music the soloist is using, to control the performance of a digitized
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6016942abffe76d28ffd1b5cff3dee2a
https://doi.org/10.1121/1.414769
https://doi.org/10.1121/1.414769
Autor:
Daniel W. Banks, John W. Paulson
Publikováno v:
Journal of Aircraft. 22:277-282
Providing next-generation fighter aircraft with short takeoff and landing capability will require effective highlift systems, methods of providing adequate longitudinal trim and control, and thrust reversers compatible with advanced configurations. R
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::612e815d26627b2e620e13e2410a788b
https://doi.org/10.2514/3.45120
https://doi.org/10.2514/3.45120