Ducted Fan Effect on the Elevation of a Concept Helicopter When the Ducted Faintail Is Located in a Ground Effect Region-Reference-Cited by-同舟云学术

Ducted Fan Effect on the Elevation of a Concept Helicopter When the Ducted Faintail Is Located in a Ground Effect Region

Published:2016-01 Issue:1 Volume:29 Page:04015030
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Doğru M. H.¹,Güzelbey İ. H.²,Göv İbrahim³

Affiliation:

1. Instructor, Dept. of Pilotage, Aircraft and Aerospace Engineering Faculty, Gaziantep Univ., Gaziantep 27310, Turkey (corresponding author).

2. Professor, Dept. of Mechanical Engineering, Engineering Faculty, Gaziantep Univ., Gaziantep 27310, Turkey.

3. Assistant Professor, Dept. of Aircraft and Aerospace Engineering, Aircraft and Aerospace Engineering Faculty, Gaziantep Univ., Gaziantep 27310, Turkey.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000519

Reference15 articles.

1. Abrego A. I. and Bulaga R. W. (2002). “Performance study of a ducted fan system.” American Helicopter Society Aerodynamics Acoustics and Test and Evaluation Technical Specialists Meeting San Francisco.

2. Performance prediction and flowfield analysis of rotors in hover, using a coupled Euler/boundary layer method

3. Numerical simulation of turbulent flow around helicopter ducted tail rotor

4. Effects of blade tip modifications on wind turbine performance using vortex model

5. Aerodynamics of cross-flow fans and their application to aircraft propulsion and flow control

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