Search U.S. government technical reports digitized or harvested by TRAIL.
Altitude-Wind-Tunnel Investigation of a 3000-Pound-Thrust Axial-Flow Turbojet Engine 3 - Analysis of Combustion-Chamber Performance
Combustion-Chamber Performance Characteristics of a Python Turbine-Propeller Engine Investigated in Altitude Wind Tunnel
Performance of basic XJ79-GE-1 turbojet engine and its components
Performance of Basic XJ79-GE-1 Turbojet Engine and Its Components