Three-Dimensional Laminar-Separation Bubble on a Cambered Thin Wing at Low Reynolds Numbers-Reference-Cited by-同舟云学术

Three-Dimensional Laminar-Separation Bubble on a Cambered Thin Wing at Low Reynolds Numbers

Published:2013-01 Issue:1 Volume:50 Page:152-163
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Chen Z. J.¹,Qin N.¹,Nowakowski A. F.¹

Affiliation:

1. Department of Mechanical Engineering, University of Sheffield, Sheffield, England S1 3JD, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C031829

Reference22 articles.

1. Challenges Facing Future Micro-Air-Vehicle Development

2. Laminar-Turbulent Transition of a Low Reynolds Number Rigid or Flexible Airfoil

3. Planform and Camber Effects on the Aerodynamics of Low-Reynolds-Number Wings

4. ObaraC. J.HolmesB. J. “Flight Measured Laminar Boundary-Layer Transition Phenomena Including Stability Theory Analysis,” NASA Technical Paper 2417, 1985.

5. Visualization of Transition in the Flow over an Airfoil Using the Smoke-Wire Technique

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