Search
Search U.S. government technical reports digitized or harvested by TRAIL.
Keyword Search
13 results returnedSearch results
- 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
- Free-flight measurements of aerodynamic heat transfer to Mach number 3.9 and of drag to Mach number 6.9 of a fin-stabilized cone-cylinder configuration
- Theoretical analysis of the longitudinal behavior of an automatically controlled supersonic interceptor during the attack phase against maneuvering and nonmaneuvering targets
- A simplified method for approximating the transient motion in angles of attack and sideslip during a constant rolling maneuver
- A flight and analytical study of methods for reducing automatic-interceptor tracking errors caused by target maneuvers
- Theoretical analysis of total-pressure loss and airflow distribution for tubular turbojet combustors with constant annulus and liner cross-sectional areas
- Survey of hydrogen combustion properties
- Flutter at very high speeds
- Theoretical rocket performance of JP-4 fuel with several fluorine-oxygen mixtures assuming frozen composition
- Performance of basic XJ79-GE-1 turbojet engine and its components
- Investigation of fixed-geometry supersonic inlets with bypass ducts for matching turbojet-engine air-flow requirements over a range of transonic and supersonic speeds