Low Reynolds number multirotor aerodynamic wake interactions-Reference-Cited by-同舟云学术

Low Reynolds number multirotor aerodynamic wake interactions

Published:2019-04 Issue:4 Volume:60 Page:
ISSN:0723-4864
Container-title:Experiments in Fluids
language:en
Short-container-title:Exp Fluids

Author:

Shukla Dhwanil^ORCID,Komerath Narayanan^ORCID

Funder

Vertical Lift Rotorcraft Centers of Excellence

Publisher

Springer Science and Business Media LLC

Subject

Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanics of Materials,Computational Mechanics

Link

http://link.springer.com/content/pdf/10.1007/s00348-019-2724-3.pdf

Reference25 articles.

1. Bagai A, Leishman JG (1996) Free-wake analysis of tandem, tilt-rotor and coaxial rotor configurations. J Am Helicopter Soc 41(3):196–207

2. Bauer AB (1975) The laminar airfoil problem. Eighth national free flight society symposium. National Free Flight Society, Lake Charles, pp 40–45

3. Bohorquez F, Pines D (2003) Hover performance of rotor blades at low reynolds numbers for rotary wing micro air vehicles. In: 2nd AIAA “Unmanned Unlimited” Conf. and Workshop & Exhibit

4. Bohorquez F, Pines D, Samuel PD (2010) Small rotor design optimization using blade element momentum theory and hover tests. J Aircr 47(1):268–283

5. Bruining A (1979) Aerodynamic characteristics of a curved plate airfoil section at Reynolds numbers 60000 and 100000 and angles of attack from − 10 to + 90 degrees. Delft University of Techology, Department of Aerospace Engineering, Report LR-281

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