Search
Search U.S. government technical reports digitized or harvested by TRAIL.
Keyword Search
15 results returnedSearch results
- Altitude-Wind-Tunnel Investigation of Performance of Several Propellers on YP-47M Airplane at High Blade Loading 2 - Curtiss 838-1C2-18R1 Four-Blade Propeller
- Preliminary Results of an Altitude-Wind-Tunnel Investigation of a TG-100A Gas Turbine-Propeller Engine 4 - Compressor and Turbine Performance Characteristics
- Preliminary Results of an Altitude-Wind-Tunnel Investigation of an Axial-Flow Gas Turbine-Propeller Engine 4 - Compressor and Turbine Performance Characteristics
- Reynolds number effect on axial-flow compressor performance
- Effect of compressor-outlet bleedoff on turbojet-engine performance
- Full-scale investigation of cooling shroud and ejector nozzle for a turbojet engine: afterburner installation
- Experimental investigation of typical constant- and variable-area exhaust nozzles and effects on axial-flow turbojet-engine performance
- Generalization of Turbojet and Turbine-Propeller Engine Performance in Windmilling Condition
- Investigation of afterburner performance and afterburner fuel system coking of the Westinghouse XJ34-WE-32 engine
- Effect of uneven air-flow distribution to the twin inlets of an axial-flow turbojet engine
- Preliminary Data on the Effects of Inlet Pressure Distortions on the J57-P-1 Turbojet Engine
- Preliminary Altitude Operational Characteristics of a J57-P1 Turbojet Engine
- Surge-Inception Study in a Two-Spool Turbojet Engine
- Surge-Inception Study in a Two-Spool Turbojet Engine, Revised
- A study of temperature transients at the inlet of a turbojet engine