Lift and Tip Vortices Generated by Tapered Backward-Swept and Forward-Swept Wings under Stationary Ground Proximity-Reference-Cited by-同舟云学术

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Lift and Tip Vortices Generated by Tapered Backward-Swept and Forward-Swept Wings under Stationary Ground Proximity

Published:2023-09 Issue:5 Volume:36 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Lin G.¹,Lee T.²

Affiliation:

1. Graduate Research Assistant, Dept. of Mechanical Engineering, McGill Univ., 817 Sherbrooke St. W., Montreal, QC, Canada H3A 2K6 (corresponding author).

2. Associate Professor, Dept. of Mechanical Engineering, McGill Univ., 817 Sherbrooke St. W., Montreal, QC, Canada H3A 2K6.

Publisher

American Society of Civil Engineers (ASCE)

Subject

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

Link

https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-5054

Reference24 articles.

1. Flow Studies of the Leading Edge Stall on a Swept-Back Wing at High Incidence

2. Vortical Flowfield Structure at Forward Swept-Wing Configurations

3. Numerical simulation of DLR-F6 wing-body flow field in ground effect

4. Wind Tunnel Measurements of Rolling Moment in a Swept-Wing Vortex Wake

5. Near-field tip vortex behind a swept wing model

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