Search U.S. government technical reports digitized or harvested by TRAIL.
Wind Tunnel Standardization Disk Drag
Pressure Distribution Over a Rectangular Monoplane Wing Model Up to 90 Degree Angle of Attack
Wind Tunnel Tests on Autorotation and The "Flat Spin"
Preliminary Report on the Flat-Top Lift Curve as a Factor in Control at Low Speed
Wind Tunnel Tests on Airfoil Boundary Control Using a Backward Opening Slot (1929)
Wind Tunnel Tests on a Model of a Monoplane Wing with Floating Ailerons
Rolling Moments Due to Rolling and Yaw for Four Wing Models in Rotation
Span load distribution on two monoplanes wing models as affected by twist and sweepback
Refrigerated wind tunnel tests on surface coatings for preventing ice formation
The Effect of Wing Tip Floating Ailerons on the Autorotation of a Monoplane Wing Model
Span-load distribution as a factor in stability in roll