A FIRST APPROXIMATION CALCULATION OF AIR CUSHION CHASSIS WEIGHT OF TRANSPORT AIRPLANE
Abstract
This article describes a first approximation of a weighted estimate of air cushion chassis. The algorithm for calculating the weight of air cushion chassis allows not only to estimate the mass of the chassis to a first approximation, but also to conduct a preliminary analysis of the influence of various parameters of the aircraft and the chassis on the weight of the aircraft at the stage of before designing. The algorithm can be expanded to include additional design decisions, such as the transformation of the fuselage, increasing the air cushion chassis canopy due to extensions, center of gravity, etc.
About the Authors
V. P. Morozov
ООО Предприятие "АЭРОРИК"
Russian Federation
Russian Federation
Y. Y. Merzlikin
"ФГУП" ЦАГИ
Russian Federation
Russian Federation
References
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Review
For citations:
Morozov V.P., Merzlikin Y.Y. A FIRST APPROXIMATION CALCULATION OF AIR CUSHION CHASSIS WEIGHT OF TRANSPORT AIRPLANE. Civil Aviation High Technologies. 2016;(223):174-180. (In Russ.)
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