Low Reynolds Number Acceleration of Flat Plate Wings at High Incidence (Invited)-Reference-Cited by-同舟云学术

Low Reynolds Number Acceleration of Flat Plate Wings at High Incidence (Invited)

Published:2016-01-02 Issue: Volume: Page:
ISSN:
Container-title:54th AIAA Aerospace Sciences Meeting
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Author:

Stevens Robbie J.¹,Babinsky Holger¹,Manar Field²,Mancini Peter²,Jones Anya R.²,Granlund Kenneth O.³,Ol Michael V.⁴,Nakata Toshiyuki⁵,Phillips Nathan⁵,Bomphrey Richard⁵,Gozukara Arif⁶

Affiliation:

1. University of Cambridge

2. University of Maryland, College Park

3. North Carolina State University

4. Air Force Research Laboratory

5. Royal Veterinary College

6. ASELSAN, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-0286

Reference9 articles.

1. 2Morgan, C., Unsteady Vortex Interactions Related to a Formula One Car Front Wing and Wheel, Ph.D. thesis,University of Cambridge,

2. Integrated modeling of insect flight: From morphology, kinematics to aerodynamics

3. A Computational Study of a Canonical Pitch-Up, Pitch-Down Wing Maneuver

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