Zobrazeno 1 - 10
of 45
pro vyhledávání: '"Edward A. Whalen"'
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
Publikováno v:
AIAA Journal. 57:3111-3114
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::faa7d1a06c0e0564d4482a9001157904
https://doi.org/10.2514/1.j058507
https://doi.org/10.2514/1.j058507
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:
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. 56:3399-3413
Thermal active flow control has been developed to enhance the efficiency of active flow control systems. The actuation concept is derived from gas-dynamics principles, and it is based on thermal control of the air supply. It is shown that higher air
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1b3dce28953c40d63c97347c5e63f106
https://doi.org/10.2514/1.j056944
https://doi.org/10.2514/1.j056944
Publikováno v:
8th AIAA Flow Control Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ce2dfd204abfb1a427d4787131e7bde2
https://doi.org/10.2514/6.2016-3306
https://doi.org/10.2514/6.2016-3306
Autor:
Paul Vijgen, Marc Spoor, Edward A. Whalen, Marlyn Y. Andino, John Tran, Arvin Shmilovich, John C. Lin
Publikováno v:
8th AIAA Flow Control Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cade4d6115af9f8a8eac8ee59d195583
https://doi.org/10.2514/6.2016-3927
https://doi.org/10.2514/6.2016-3927
Autor:
Marlyn Y. Andino, Edward A. Whalen, Marc Spoor, Michael G. Alexander, John C. Lin, John Tran, Israel Wygnanski
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
This paper summarizes a joint NASA/Boeing research effort to advance Active Flow Control (AFC) technology to enhance aerodynamic efficiency of a vertical tail. Sweeping jet AFC technology was successfully tested on subscale and full-scale models as w
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::32b1892694308ffc69c00cebc6dd25c2
https://doi.org/10.2514/6.2016-0056
https://doi.org/10.2514/6.2016-0056
Autor:
Jenna L. Eppink, Marlyn Y. Andino, Michael G. Alexander, Edward A. Whalen, John C. Lin, Emilie J. Siochi
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
This paper highlights the technology development of two flow control concepts for aircraft drag reduction. The NASA Environmentally Responsible Aviation (ERA) project worked with Boeing to demonstrate these two concepts on a specially outfitted Boein
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2bfa60b5507d67fd0b61df7827b10d97
https://doi.org/10.2514/6.2016-0864
https://doi.org/10.2514/6.2016-0864
Publikováno v:
Encyclopedia of Aerospace Engineering
Two approaches for aircraft drag reduction are reviewed. Laminar flow control has long been studied as a potential drag reduction approach with a promise to reduce fuel burn by over 10%, but it is beginning to appear in a small way on modern commerci
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2001bb297d4b887e1c3f46e8ec210157
https://doi.org/10.1002/9780470686652.eae1013
https://doi.org/10.1002/9780470686652.eae1013
