Single rotor helicopter parasite drag estimation in the preliminary design stage

Single rotor helicopter parasite drag estimation in the preliminary design stage

This paper presents the methodology for the rapid estimation of the single rotor helicopter parasite drag in the forward flight in the preliminary design phase. The aerodynamic drag of fuselage, main rotor hub, landing gear and the other, non-rotating defective surfaces contribute with more than 50%...

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Bibliographic Details
Main Authors: Dodić Marjan D., Krstić Branimir B., Rašuo Boško P.
Format: Article
Language:English
Published: Savez inženjera i tehničara Srbije 2018-01-01
Series:Tehnika
Subjects:
helicopter parasite drag
performance
preliminary design phase
equivalent parasite dragflat plate area
power required
forward flight
Online Access:https://scindeks-clanci.ceon.rs/data/pdf/0040-2176/2018/0040-21761801065D.pdf

Internet

https://scindeks-clanci.ceon.rs/data/pdf/0040-2176/2018/0040-21761801065D.pdf

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