Computational Investigation of Varying Plate-Line Geometry and Placement on Wake Vortex Dissipation-Reference-Cited by-同舟云学术

Computational Investigation of Varying Plate-Line Geometry and Placement on Wake Vortex Dissipation

Author:

Wang C. H. John¹,Zhao Dan²,Schlüter Jörg³,Stephan Anton⁴,Holzäpfel Frank⁴

Affiliation:

1. Nanyang Technological University, Singapore 639798, Republic of Singapore

2. University of Canterbury, Christchurch 8140, New Zealand

3. Deakin University, Geelong, Victoria 3220, Australia

4. DLR, German Aerospace Center, 82234 Oberpfaffenhofen, Germany

Funder

Singapore Air Traffic Management Research Institute

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

Reference43 articles.

1. “Procedures for Air Navigation Service: Air Traffic Management,” International Civil Aviation Organization, Montreal, Canada, 2007.

2. “Aircraft Type Designators,” International Civil Aviation Organization Rept. 8643, Montreal, Canada, 1996.

3. “RECAT-EU European Wake Turbulence Categorisation and Separation Minima on Approach and Departure,” Eurocontrol, Brussels, Belgium, 2015.

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2. Numerical studies on modeling the near- and far-field wake vortex of a quadrotor in forward flight;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-01-25