Search U.S. government technical reports digitized or harvested by TRAIL.
Lead Susceptibility of Several Fuels as Determined in an Air-Cooled Aircraft-Engine Cylinder
Langley Full-Scale Tunnel Investigation of a 1/3-Scale Model of the Chance Vought XF5U-1 Airplane
A Photographic Profile Recorder for Airscrews and Wing Models
The Supersonic Axial-Flow Compressor
On the Problem of Stress Corrosion
Variation with Mach Number of Static and Total Pressures Through Various Screens
Wind-Tunnel Investigation of the Horizontal Motion of a Wing Near the Ground
Analysis of Effect of Rolling Pull-Outs on Wing and Aileron Loads of a Fighter Airplane
High-Speed Wind-Tunnel Tests of a Twin-Fuselage Pursuit Airplane
Hydraulic Characteristics of the NACA Injection Impeller
Free-Spinning-Tunnel Tests of a 1/26th Scale Model of the Douglas XTB2D-1 Airplane
Ground-Stand Cooling Investigation of an R-2600-22 Engine in a PBM-3D Nacelle
Investigation of the Behavior of Thin-Walled Panels with Cutouts
Theoretical and Experimental Data for a Number of NACA 6A-Series Airfoil Sections
Method for calculating wing characteristics by lifting-line theory using nonlinear section lift data
Tank Tests of an Alternate Hull Form for the Consolidated Vultee PB2Y-3 Airplane
Field of Flow About a Jet and Effect of Jets on Stability of Jet-Propelled Airplanes
Internal and external aerodynamics of ducted bodies at supersonic speeds
Standard nomenclature for airspeeds with tables and charts for use in calculation of airspeed
Waters Loads on the XJL-1 Hull as Obtained in Langley Impact Basin, TED No. NACA 2413.3