1. Large-amplitude high-rate roll experiments on a delta and double delta wing
2. Huang, X. "IAR program on maneuvering aerodynamics over military wing configurations", To be published in 2003. Table 1: Wind tunnel or watertunnel entries
3. Year Tunnel Configuration Motion Measurements
4. 1996~1997 IAR 15x20 water tunnel 50°~79° delta wing Static in roll and pitch Off-surface flow vis.
5. 1998~1999 IAR 15x20 Water tnnel 65°, 70° delta wing Static pitch Off-surface flow vis.