Study on the influence of Leading-edge gap with drooped spoiler on civil aircraft

Guardado en:
Detalles Bibliográficos
Publicado en:Journal of Physics: Conference Series vol. 2955, no. 1 (Feb 2025), p. 012005
Autor principal: Cheng, Changfu
Otros Autores: Liu, Cangsong, Mao, Jun, Wu, Dawei
Publicado:
IOP Publishing
Materias:
Acceso en línea:Citation/Abstract
Full Text - PDF
Etiquetas: Agregar Etiqueta
Sin Etiquetas, Sea el primero en etiquetar este registro!

MARC

LEADER 00000nab a2200000uu 4500
001 3166749566
003 UK-CbPIL
022 |a 1742-6588 
022 |a 1742-6596 
024 7 |a 10.1088/1742-6596/2955/1/012005  |2 doi 
035 |a 3166749566 
045 2 |b d20250201  |b d20250228 
100 1 |a Cheng, Changfu 
245 1 |a Study on the influence of Leading-edge gap with drooped spoiler on civil aircraft 
260 |b IOP Publishing  |c Feb 2025 
513 |a Journal Article 
520 3 |a For the Adaptive Dropped Hinge Flap (ADHF), there exists a gap between the spoiler and the fixed wing when the spoiler is deflected, which affects the aerodynamic characteristics of the airplane. Numerical simulations are conducted on multi-segment wings with a deflected spoiler, focusing on the aerodynamic effects of the gap around multi-segment airfoils with spoiler deflection. The results show that the gap of the drooped spoiler has a significant influence on the characteristics of lift and drag, reducing the lift line slope of the linear segment, and decreasing the maximum lift coefficient. Also, the presence of the gap causes the stall angle of attack to decrease. Additionally, this effect diminishes with the decrease in the deflection angle of the spoiler. 
653 |a Aerodynamic coefficients 
653 |a Segments 
653 |a Angle of attack 
653 |a Wings (aircraft) 
653 |a Spoilers 
653 |a Aerodynamic characteristics 
653 |a Deflection 
700 1 |a Liu, Cangsong 
700 1 |a Mao, Jun 
700 1 |a Wu, Dawei 
773 0 |t Journal of Physics: Conference Series  |g vol. 2955, no. 1 (Feb 2025), p. 012005 
786 0 |d ProQuest  |t Advanced Technologies & Aerospace Database 
856 4 1 |3 Citation/Abstract  |u https://www.proquest.com/docview/3166749566/abstract/embedded/7BTGNMKEMPT1V9Z2?source=fedsrch 
856 4 0 |3 Full Text - PDF  |u https://www.proquest.com/docview/3166749566/fulltextPDF/embedded/7BTGNMKEMPT1V9Z2?source=fedsrch