Search U.S. government technical reports digitized or harvested by TRAIL.
An experimental investigation of NACA submerged air inlets on a 1/5-scale model of a fighter airplane
Boundary-layer and stalling characteristics of the NACA 63-009 airfoil section
An experimental investigation of regions of separated laminar flow
An investigation at low speed of the flow over a simulated flat plate at small angles of attack using pitot-static and hot-wire probes
A correlation of low-speed, airfoil-section stalling characteristics with Reynolds number and airfoil geometry