Search U.S. government technical reports digitized or harvested by TRAIL.
Theoretical wave drags and pressure distributions for axially symmetric open-nose bodies
Low-speed investigation of the stalling of a thin, faired, double-wedge airfoil with nose flap
A method of determining the effect of airplane stability on the gust load factor
Method of experimentally determining radial distributions of velocity through axial-flow compressor
Formulas for source, doublet, and vortex distributions in supersonic wing theory
The interpretation of biaxial-tension experiments involving constant stress ratios
Approximate aerodynamic influence coefficients for wings of arbitrary plan form in subsonic flow
Frequency response of positive-displacement variable stroke fuel pump
Critical stress of plate columns
A comparison of theoretical and experimental wing bending moments during seaplane landings
Investigation of spark-over voltage - density relation for gas-temperature sensing
Application of the wire-mesh plotting device to incompressible cascade flows
Relation Between Inflammables and Ignition Sources in Aircraft Environments
A flight investigation and analysis of the lateral-oscillation characteristics of an airplane
Stress and strain concentration at a circular hole in an infinite plate
Spectrums and diffusion in a round turbulent jet
The calculation of downwash behind wings of arbitrary plan form at supersonic speeds
Theoretical analysis of various thrust-augmentation cycles for turbojet engines
Density fields around a sphere at Mach numbers 1.30 and 1.62
Maximum pitching angular accelerations of airplanes measured in flight
Gust-tunnel investigation of a wing model with semichord line swept back 60 degrees
Charts of thermodynamic properties of air and combustion products from 300 degrees to 3500 degrees R
Properties of a boron carbide-iron ceramal
Sintering mechanism between zirconium carbide and columbium
General method for computation of equilibrium composition and temperature of chemical reactions
Tables of thermodynamic functions for analysis of aircraft-propulsion systems