Aerodynamic Characteristics of a Swept Wing in Close Ground Proximity at High Subsonic Mach Numbers-Reference-Cited by-同舟云学术

Aerodynamic Characteristics of a Swept Wing in Close Ground Proximity at High Subsonic Mach Numbers

Published:2012-10 Issue:4 Volume:25 Page:600-612
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Doig Graham¹,Barber Tracie J.²,Neely Andrew J.³

Affiliation:

1. Associate Lecturer, School of Mechanical and Manufacturing Engineering, Univ. of New South Wales, Kensington, Sydney, NSW 2052, Australia (corresponding author).

2. Associate Professor, School of Mechanical and Manufacturing Engineering, Univ. of New South Wales, Kensington, Sydney, NSW 2052, Australia.

3. Associate Professor, School of Engineering and Information Technology, Australian Defense Force Academy, Univ. of New South Wales, 2600 Northcott Dr., Canberra, ACT 2600, Australia.

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.1943-5525.0000169

Reference17 articles.

1. Causes for discrepancies in ground effect analyses;Barber T. J.;Aeronaut. J.,2002

2. Numerical solution of the equation for a thin airfoil in ground effect

3. A direct boundary integral equations method to subsonic flow with circulation past thin airfoils in ground effect

4. Fully Three-Dimensional Transition Prediction on Swept Wings in Transonic Flows

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