Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Seung Yeun Yoo"'
Weak-value amplification (WVA) provides a way for amplified detection of a tiny physical signal at the expense of a lower detection probability. Despite this trade-off, due to its robustness against certain types of noise, WVA has advantages over con
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::cc3d3948856fce8a5fe37cdb80652939
Autor:
Seung Yeun Yoo
Publikováno v:
Journal of Aircraft. 50:354-359
The streamwise lift distribution of a wing-canard-stabilator-body configuration was varied to study its effect on the near-field sonic boom signature. The investigation was carried out via solving the three-dimensional Euler equation with the OVERFLO
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2368ebdf9d550ac1cf5f0e90d3d76683
https://doi.org/10.2514/1.c031517
https://doi.org/10.2514/1.c031517
Autor:
Walter A. Silva, Mark D. Sanetrik, Michael Buonanno, Pawel Chwalowski, Paul Scott Zink, Seung Yeun Yoo, David M. Christhilf, Antonio De La Garza, James R. Florance, J. C. Johnson, George Kopasakis, Jiyoung Hur, Elias G. Bounajem
Publikováno v:
56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
An overview of NASA’s High Speed Aeroservoelasticity (ASE) project is provided with a focus on recent computational aeroelastic analyses of a low-boom supersonic configuration developed by Lockheed-Martin and referred to as the N+2 configuration. T
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6cd543240b59406f3fbe73c6519bfb5f
https://doi.org/10.2514/6.2015-0684
https://doi.org/10.2514/6.2015-0684
Publikováno v:
AIAA Guidance, Navigation, and Control Conference.
This paper focuses on the development of an intelligent control technology for in-flight drag reduction. The system is integrated with and demonstrated on the full X-48B nonlinear simulation. The intelligent control system utilizes a peak-seeking con
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2f610e74425050c5ce3fd268c33d1719
https://doi.org/10.2514/6.2011-6470
https://doi.org/10.2514/6.2011-6470
Autor:
Brian R. Taylor, Seung Yeun Yoo
Publikováno v:
AIAA Guidance, Navigation, and Control Conference.
Asymmetric engine thrust was implemented in a hybrid-wing-body non-linear simulation to reduce the amount of aerodynamic surface deflection required for yaw stability and control. Hybrid-wing-body aircraft are especially susceptible to yaw surface de
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::92085f8049d1860a60d9a75ffa7056fa
https://doi.org/10.2514/6.2011-6253
https://doi.org/10.2514/6.2011-6253
Publikováno v:
46th AIAA Aerospace Sciences Meeting and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d95ce7c19baa584c8d1da2aafec507c3
https://doi.org/10.2514/6.2008-1332
https://doi.org/10.2514/6.2008-1332
Publikováno v:
Physical Review Letters. 1/28/2022, Vol. 128 Issue 4, p1-1. 1p.