reverse taper
Recently Published Documents


TOTAL DOCUMENTS

24
(FIVE YEARS 7)

H-INDEX

4
(FIVE YEARS 1)

2021 ◽  
Author(s):  
Jae Ha Ryu ◽  
Benjamin Knipfer ◽  
Jeremy D. Kirch ◽  
Robert A. Marsland ◽  
Steve Jacobs ◽  
...  

Photonics ◽  
2021 ◽  
Vol 8 (2) ◽  
pp. 44
Author(s):  
Kaiqing Zhang ◽  
Tao Liu ◽  
Zheng Qi ◽  
Xiaoxi Fu ◽  
Chao Feng ◽  
...  

External seeded free-electron lasers (FELs) hold promising prospects for producing intense coherent radiation at high harmonics of a conventional laser. The practical harmonic up-conversion efficiencies of current seeding techniques are limited by various three-dimensional effects on the electron beam. In this paper, a novel method is proposed to extend the wavelength coverage of a seeded FEL by combining the reverse taper undulator with the echo-enabled harmonic generation. The proposed technique can significantly enhance the bunching at ultra-high harmonics and preserve the electron beam qualities from degradation by deleterious effects. Theoretical analysis and numerical simulation are performed, and the results demonstrate that stable, intense, nearly fully coherent FEL pulses with photon energy up to 1 keV can be generated. The proposed technique may open up new opportunities to obtain laser-like pulses at sub-nanometer wavelength.


2020 ◽  
Vol 8 (3) ◽  
pp. 156 ◽  
Author(s):  
Saeed Jamei ◽  
Adi Maimun ◽  
Rasul Niazmand Bilandi ◽  
Nor Azwadi ◽  
Simone Mancini ◽  
...  

Flow structure is a crucial point for the conceptual design of Wing-in-Ground effect (WIG) crafts. In this study, pressure distributions around a compound wing, velocity and the turbulent intensity distribution in the wake area after trailing of the wing, have been investigated numerically. Computational simulations were completed regarding various angles of attack in-ground-effect. Two parts made up the compound wing: The first composed by one rectangular wing in the center, the second composed by a reverse taper wing, consisting of an anhedral angle at the side. A realizable k-ε turbulent model exhibited the flow field in the physical domain about the wing surface. The numerical results of the compound wing were validated using the data provided by wind tunnel tests. The flow structures around the compound wing were compared with that of a rectangular wing for different conditions. It was found that the pressure distribution on the rectangular wing was weaker than at the lower surface for the compound wing. However, the suction effect on the upper surface of the rectangular wing was higher. Also, the velocity defect and the turbulence level in the wake area was greater behind the compound wing.


2019 ◽  
Vol 30 (S19) ◽  
pp. 232-232
Author(s):  
Jeremy Pitman ◽  
Maarten Glibert ◽  
Hugo De Bruyn ◽  
Veronique Christiaens
Keyword(s):  
The Self ◽  

Author(s):  
Мещеряков ◽  
Sergey Meshcheryakov ◽  
Романович ◽  
Aleksey Romanovich ◽  
Воронов ◽  
...  

The article describes the design of a pilot plant PVI includes a feed hopper mounted on the frame of the conical rolls and designersusa device, which consists of additional rolls with a reverse taper rolls the main. allows to combine the processes of comminution and disaggregation of compressed materi-als. We theoretically studied the implementation of directional movement pressed into the plate material from the main to the additional rolls desagglomeration device. Presents an analysis of the graphic curves constructed according to the obtained equations for the linear size of the capture zone dezagregarea rolls plates of pressed material. It is concluded that the intensive change of the angle is on the interval from zero to 0.25 meters, which should be taken into account when designing the press roller cutter device for desagglomeration materials.


2015 ◽  
Vol 5 (1) ◽  
Author(s):  
Sebastian W. Schmitt ◽  
George Sarau ◽  
Silke Christiansen

Abstract Silicon nanowires (SiNWs) attached to a wafer substrate are converted to inversely tapered silicon nanocones (SiNCs). After excitation with visible light, individual SiNCs show a 200-fold enhanced integral band-to-band luminescence as compared to a straight SiNW reference. Furthermore, the reverse taper is responsible for multifold emission peaks in addition to the relatively broad near-infrared (NIR) luminescence spectrum. A thorough numerical mode analysis reveals that unlike a SiNW the inverted SiNC sustains a multitude of leaky whispering gallery modes. The modes are unique to this geometry and they are characterized by a relatively high quality factor (Q ~ 1300) and a low mode volume (0.2 < (λ/neff)3 < 4). In addition they show a vertical out coupling of the optically excited NIR luminescence with a numerical aperture as low as 0.22. Estimated Purcell factors Fp ∝ Q/V m of these modes can explain the enhanced luminescence in individual emission peaks as compared to the SiNW reference. Investigating the relation between the SiNC geometry and the mode formation leads to simple design rules that permit to control the number and wavelength of the hosted modes and therefore the luminescent emission peaks.


Sign in / Sign up

Export Citation Format

Share Document