Search
Search U.S. government technical reports digitized or harvested by TRAIL.
Keyword Search
10 results returnedSearch results
- Efficiency tests of a single-stage impulse turbine having an 11.0-inch pitch-line diameter wheel with air as the driving fluid
- The Performance of a Single-Stage Impulse Turbine Having an 11.0-Inch Pitch-Line Diameter Wheel with Cast Airfoil-Shaped and Bent Sheet-Metal Nozzle Blades
- The effect of two inlet-duct designs on turbine efficiency
- The Effect of Inlet Pressure and Temperature on the Efficiency of a Single Stage Impulse Turbine Having an 11.0-Inch Pitch-Line Diameter Wheel
- Experimental investigation of performance and operating characteristics of a tail-pipe burner for a turbojet engine
- Analytical and experimental investigation of thrust augmentation of axial- and centrifugal-compressor turbojet engines by injection of water and alcohol in combustion chambers
- Experimental Study of Isothermal Wake-Flow Characteristics of Various Flame-Holder Shapes
- Analysis of the turbojet engine for propulsion of supersonic fighter airplanes
- A survey of methods for turbojet thrust measurement applicable to flight installation
- Summary of NACA research on afterburners for turbojet engines