Zobrazeno 1 - 10
of 33
pro vyhledávání: '"Marlyn Y. Andino"'
Autor:
John C. Lin, LaTunia G. Pack Melton, Judith A. Hannon, Mehti Koklu, Keith B. Paschal, Veer N. Vatsa, Marlyn Y. Andino
Publikováno v:
AIAA Journal. 59:3748-3763
A 10%-scale high-lift version of the Common Research Model (CRM-HL) was tested in the NASA Langley Research Center’s 14 by 22 ft subsonic tunnel. The focus of the wind-tunnel tests was to investiga...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ed3d2dee1ccb968ecaf885c5ef9d9da7
https://doi.org/10.2514/1.j059869
https://doi.org/10.2514/1.j059869
Autor:
Keith B. Paschal, Mehti Koklu, Veer N. Vatsa, Judith A. Hannon, LaTunia G. Pack Melton, John C. Lin, Marlyn Y. Andino
Publikováno v:
Journal of Aircraft. 57:1121-1133
A 10%-scale high-lift version of the Common Research Model and an active flow control (AFC) version of the model equipped with a simple-hinged flap were successfully tested. The main objective of t...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f36bede828dd6d46e6700594733f2550
https://doi.org/10.2514/1.c035906
https://doi.org/10.2514/1.c035906
Autor:
Edward A. Whalen, Seele Roman, Israel Wygnanski, Marlyn Y. Andino, Mory Gharib, Emilio Graff, John C. Lin
Publikováno v:
AIAA J
Active flow control (AFC) subscale experiments were conducted at the Lucas Wind Tunnel of the California Institute of Technology. Tests were performed on a generic vertical tail model at low speeds. Fluidic oscillators were used at the trailing edge
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::409bc37dc53360a60b87fefd72d88551
https://doi.org/10.2514/1.j057876
https://doi.org/10.2514/1.j057876
Autor:
Anthony E. Washburn, John C. Lin, Emilio Graff, Marlyn Y. Andino, Israel Wygnanski, Edward A. Whalen, Morteza Gharib, Douglas S. Lacy
Publikováno v:
Journal of Aircraft. 56:1376-1386
Full-scale wind tunnel tests were carried out on a Boeing 757 vertical tail equipped with 37 sweeping jet actuators on the starboard side along the rudder hinge line. The tests were performed at th...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2641453c4dcca37cdd055c160da65834
https://doi.org/10.2514/1.c034907
https://doi.org/10.2514/1.c034907
Autor:
Keith C. Paschal, Veer N. Vatsa, Mehti Koklu, John C. Lin, LaTunia G. Pack Melton, Marlyn Y. Andino, Judith A. Hannon
Publikováno v:
AIAA Scitech 2020 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1007c80b9f356952ef02f6afe92a47cd
https://doi.org/10.2514/6.2020-0783
https://doi.org/10.2514/6.2020-0783
Autor:
John C. Lin, Keith C. Paschal, Judith A. Hannon, Mehti Koklu, LaTunia G. Pack Melton, Veer N. Vatsa, Marlyn Y. Andino
Publikováno v:
AIAA Scitech 2020 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f556ddb377f866301dbc97a13eca84e3
https://doi.org/10.2514/6.2020-0786
https://doi.org/10.2514/6.2020-0786
Autor:
Paul Vijgen, Marc Spoor, John C. Lin, John Tran, Edward A. Whalen, Arvin Shmilovich, Marlyn Y. Andino
Publikováno v:
AIAA Journal. 56:3393-3398
The size of the vertical tail and rudder of a commercial aircraft is influenced by the requirement that the airplane must be controllable in the event of an engine failure. As a result, on twin-eng...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0b5e6e6d310d7576b0e4b59c3147c898
https://doi.org/10.2514/1.j056959
https://doi.org/10.2514/1.j056959
Publikováno v:
AIAA Journal. 56:2961-2973
Active flow control (AFC) in the form of sweeping jet (SWJ) excitation and discrete steady jet excitation is used to control the flow separation on a National Advisory Council for Aeronautics (NACA...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f1d4d95e3b12be1443de6ae6088401ba
https://doi.org/10.2514/1.j056841
https://doi.org/10.2514/1.j056841
Autor:
Judith A. Hannon, John C. Lin, Mehti Koklu, Keith B. Paschal, Marlyn Y. Andino, LaTunia G. Pack Melton
Publikováno v:
AIAA Aviation 2019 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fa14ddc4ea93e3c1c3377f4ab996db1c
https://doi.org/10.2514/6.2019-3726
https://doi.org/10.2514/6.2019-3726
Autor:
Judith A. Hannon, John C. Lin, Keith B. Paschal, LaTunia G. Pack Melton, Marlyn Y. Andino, Veer N. Vatsa, Mehti Koklu
Publikováno v:
AIAA Aviation 2019 Forum.
A 10% scale version of the High-Lift Common Research Model (CRM-HL) was tested in the NASA Langley 14- by 22-Foot Subsonic Tunnel (14x22) in support of the NASA Advanced Air Transport Technology (AATT) Project. The CRM-HL experiment included various
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1a1b3c87444da4a8ce018c27e3f4804c
https://doi.org/10.2514/6.2019-3727
https://doi.org/10.2514/6.2019-3727