Reduction of Transient Adverse Effects of Spoilers
Author:
Affiliation:
1. Nanyang Technological University, Singapore 639798, Singapore
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2216
Reference7 articles.
1. Aerodynamic characteristics of a two-dimensional moving spoiler in subsonic and transonic flow
2. Unsteady, separated flow behind an oscillating, two-dimensional spoiler
3. Detection of flow state in an unsteady separating flow
4. Aircraft spoiler effects under wind shear
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