Helical-Groove and Circular-Trip Effects on Side Force
Author:
Affiliation:
1. National University of Singapore, Singapore 119260, Republic of Singapore
2. DSO National Laboratories, Singapore 118230, Republic of Singapore
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2689
Reference19 articles.
1. Onset of aerodynamic side forces at zero sideslip on symmetric forebodies at high angles of attack
2. Keener, E. R., Chapman, G. T., and Kruse, R. L. “Effects of Mach Number and Afterbody Length on Onset of Asymmetric Forces on Bodies at Zero Sideslip and High Angle of Attack,” AIAA Paper 76-66, Jan. 1976.
3. Forebody Vortex Control as a Complement to Thrust Vectoring
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