1. Lift and Pitching Moment at Low Speeds of The NACA 64A010 Airfoil Section Equipped with Various Combinations of a Leading-Edge Slat, Leading-Edge Flap, Split Flap, and Double-Slotted Flap;NACA TN-3007,1953
2. Variable-Camber Systems Integration and Operational Performance of the AFTI/F-111 Mission Adaptive Wing;NASA TM-4370,1992
3. High-Lift Aerodynamics;Smith;Journal of Aircraft,1975
4. Study of Slat-Airfoil Combinations Using Computer Graphics;Liebeck;Journal of Aircraft,1973