1. Applications of the unsteady vortex-lattice method in aircraft aeroelasticity and flight dynamics
2. QueijoM. J. “Theoretical Span Load Distributions and Rolling Moments for Sideslipping Wings of Arbitrary Plan form in Incompressible Flow,” NACA TN-3605, 1955.
3. GoodmanA.BrewerJ. D. “Investigation at Low Speeds of the Effect of Aspect Ratio and Sweep on Static and Yawing Stability Derivatives of Untapered Wings,” NACA TN-1669, 1948.
4. LetkoW.GoodmanA. “Preliminary Wind-Tunnel Investigation at Low Speed of Stability and Control Characteristics of Swept-Back Wings,” NACA TN-1046, 1946.
5. Leading-edge flow reattachment and the lateral static stability of low-aspect-ratio rectangular wings