Search U.S. government technical reports digitized or harvested by TRAIL.
Wind-Tunnel Investigation of an NACA 23021 Airfoil With Two Sizes of Balanced Split Flaps
Determination of the Stability and Control Characteristics of Airplanes from Tests of Powered Models
Jet-Boundary Corrections to a Yawed Model in a Closed Rectangular Wind Tunnel
Jet-boundary corrections for reflection-plane models in rectangular wind tunnels
Jet-boundary corrections for reflection-plane models in rectangular wind tunnels
Limitations of lifting-line theory for estimation of aileron hinge-moment characteristics
Wind-Tunnel Calibration and Correction Procedures for Three-Dimensional Models
An Electromagnetic-Analogy Method of Solving Lifting-Surface-Theory Problems