Navier-Stokes Computation of a Rapidly Deploying Spoiler
Author:
Affiliation:
1. Korea Aerospace Research Institute, Taejon 305-333, Republic of Korea
2. Korea Advanced Institute of Science and Technology, Taejon 305-701, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2648
Reference18 articles.
1. 3Nelson, R. C., Flight Stability and Automatic Control, McGraw-Hill, NewYork, 1989, pp.207-210.
2. Aerodynamic characteristics of a two-dimensional moving spoiler in subsonic and transonic flow
3. On the prospects for increasing dynamic lift
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