Search U.S. government technical reports digitized or harvested by TRAIL.
Performance of NACA eight-stage axial-flow compressor designed on the basis of airfoil theory
The rolling moment due to sideslip of swept wings at subsonic and transonic speeds
Effect of surface roughness on characteristics of spherical shock waves
Survey of hydrogen combustion properties
Performance of basic XJ79-GE-1 turbojet engine and its components