Email this article Influence of the Air Viscosity on the Induced Power of a Helicopter Main Rotor in Hover and Vertical Takeoff Modes
- Authors: Shaidakov V.I.1, Brusov V.S.1
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Affiliations:
- Moscow Aviation Institute (National Research University)
- Issue: Vol 60, No 4 (2017)
- Pages: 567-574
- Section: Aero- and Gas-Dynamics of Flight Vehicles and Their Engines
- URL: https://journals.rcsi.science/1068-7998/article/view/230301
- DOI: https://doi.org/10.3103/S1068799817040134
- ID: 230301
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Abstract
The paper presents a method of calculating the main rotor's inductive velocities considering the influence of nonlinear air stream on ejection of air masses contiguous to it.
About the authors
V. I. Shaidakov
Moscow Aviation Institute (National Research University)
Author for correspondence.
Email: k102@mai.ru
Russian Federation, Volokolamskoe shosse 4, Moscow, 125993
V. S. Brusov
Moscow Aviation Institute (National Research University)
Email: k102@mai.ru
Russian Federation, Volokolamskoe shosse 4, Moscow, 125993
