Stress-strain state of ice cover during aircraft takeoff and landing
被引:11
作者:
Pogorelova, A. V.
论文数: 0引用数: 0
h-index: 0
机构:
Russian Acad Sci, Far Eastern Branch, Inst Engn & Met, Komsomolsk On Amur 681005, RussiaRussian Acad Sci, Far Eastern Branch, Inst Engn & Met, Komsomolsk On Amur 681005, Russia
Pogorelova, A. V.
[1
]
Kozin, V. M.
论文数: 0引用数: 0
h-index: 0
机构:
Komsomolsk On Amur State Tech Univ, Komsomolsk On Amur 681013, RussiaRussian Acad Sci, Far Eastern Branch, Inst Engn & Met, Komsomolsk On Amur 681005, Russia
Kozin, V. M.
[2
]
Matyushina, A. A.
论文数: 0引用数: 0
h-index: 0
机构:
Amur Humanitarian & Pedag State Univ, Komsomolsk On Amur 681000, RussiaRussian Acad Sci, Far Eastern Branch, Inst Engn & Met, Komsomolsk On Amur 681005, Russia
Matyushina, A. A.
[3
]
机构:
[1] Russian Acad Sci, Far Eastern Branch, Inst Engn & Met, Komsomolsk On Amur 681005, Russia
[2] Komsomolsk On Amur State Tech Univ, Komsomolsk On Amur 681013, Russia
[3] Amur Humanitarian & Pedag State Univ, Komsomolsk On Amur 681000, Russia
We consider the linear unsteady motion of an IL-76TD aircraft on ice. Water is treated as an ideal incompressible liquid, and the liquid motion is considered potential. Ice cover is modeled by an initially unstressed uniform isotropic elastic plate, and the load exerted by the aircraft on the ice cover with consideration of the wing lift is modeled by regions of distributed pressure of variable intensity, arranged under the aircraft landing gear. The effect of the thickness and elastic modulus of the ice plate, takeoff and landing regimes on stress-strain state of the ice cover used as a runway.