Linearized Lifting-surface Theory for Swept-back Wings with Slender Plan Forms / Harvard Lomax and Max A. Heaslet.Harvard. Lomax1949EN
The Calculation of Downwash Behind Supersonic Wings with an Application to Triangular Plan Forms / Max A. Heaslet and Harvard Lomax.Max A. Heaslet1948EN
Damping-in-roll Calculations for Slender Swept-back Wings and Slender Wing-body Combinations / Harvard Lomax and Max A. Heaslet.Harvard. Lomax1949EN
Volterra's Solution of the Wave Equation as Applied to Three-dimensional Supersonic Airfoil Problems / Max A. Heaslet, Harvard Lomax, and Arthur L. Jones.Max A. Heaslet1947EN