Search U.S. government technical reports digitized or harvested by TRAIL.
Effect of Mach and Reynolds Numbers on Maximum Lift Coefficient
Flight Observations of Aileron Flutter at High Mach Numbers as Affected by Several Modifications
On the Application of Transonic Similarity Rules to Wings of Finite Span
Downwash and Sidewash Fields Behind Cruciform Wings
On the Application of Transonic Similarity Rules
Theoretical Prediction of Pressure Distributions on Nonlifting Airfoils at High Subsonic Speeds
On the range of applicability of the transonic area rule
On the Range of Applicability of the Transonic Area Rule
Thin airfoil theory based on approximate solution of the transonic flow equation