Power balance of an aircraft with air-cushion undercarriage
Published: 07.11.2014
Authors: Morozov V.P., Naumov V.N., Chizhov D.A., Merzlikin Yu.Yu., Menshikov A.S.
Published in issue: #12(36)/2014
DOI: 10.18698/2308-6033-2014-12-1300
Category: Engineering | Chapter: Transport systems
The article presents an equation of power balance of the aircraft with air-cushion landing gear. It includes the total power of all engines necessary for take-off, cruise flight and air-cushion operation which are determined from the equation. A short analysis of influence of the said parameters on power of the aircraft with air-cushion undercarriage is given.
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