During a free-jet investigation of a 28-inch ram-jet engine at a Mach number of 2.35, flow pulsation at the engine inlet were discovered which proved to have an effect on the engine performance and operational characteristics, particularly the engine rich blowout limits. This report discusses the finding of the flow pulsations, their elimination, and effect. Other facility characteristics, such as the establishment of flow simulation and the degree of subcritical operation of the diffuser, are also explained
Free-flight performance of five 16-inch-diameter ram-jet units was determined over range of free-str...
Results obtained with three different burner configurations in a connected-pipe investigation of a 1...
A J34 turbojet engine was investigated at free-stream Mach numbers of 0.12 and 1.6 to 2.0 to determi...
During a free-jet investigation of a 28-inch ram-jet engine at a Mach number of 2.35, flow pulsation...
An investigation was conducted to determine the effectiveness of a free-jet diffuser in reducing the...
Experimental investigation of engine dynamics and controls for 48-inch ramjet engine in free jet fac...
Experimental study of effects of combustion roughness and controlled mechanical oscillations on diff...
Engine dynamics and controls data are presented for a ram-jet engine which was operated in a free-je...
The effects of mass-flow ratio on the additive drag and normal-shock position of a single oblique-sh...
Results are presented of free-jet tests of a 1.1-inch-diameter hydrogen-burning ram-jet engine over ...
Data obtained from the NACA air-launched ram-jet program are summarized with emphasis placed upon th...
Engine dynamics were investigated for supercritical operation of the ram jet at Mach 2.75 over a ran...
The investigation of air-launched ram-jet engines has been extended to include a study of models wit...
The dynamic response of a 28-inch-diameter ramjet engine was investigated for flight Mach numbers of...
Performance of four 16-inch-diameter ram-jet units was determined at free-stream Mach numbers of 0.4...
Free-flight performance of five 16-inch-diameter ram-jet units was determined over range of free-str...
Results obtained with three different burner configurations in a connected-pipe investigation of a 1...
A J34 turbojet engine was investigated at free-stream Mach numbers of 0.12 and 1.6 to 2.0 to determi...
During a free-jet investigation of a 28-inch ram-jet engine at a Mach number of 2.35, flow pulsation...
An investigation was conducted to determine the effectiveness of a free-jet diffuser in reducing the...
Experimental investigation of engine dynamics and controls for 48-inch ramjet engine in free jet fac...
Experimental study of effects of combustion roughness and controlled mechanical oscillations on diff...
Engine dynamics and controls data are presented for a ram-jet engine which was operated in a free-je...
The effects of mass-flow ratio on the additive drag and normal-shock position of a single oblique-sh...
Results are presented of free-jet tests of a 1.1-inch-diameter hydrogen-burning ram-jet engine over ...
Data obtained from the NACA air-launched ram-jet program are summarized with emphasis placed upon th...
Engine dynamics were investigated for supercritical operation of the ram jet at Mach 2.75 over a ran...
The investigation of air-launched ram-jet engines has been extended to include a study of models wit...
The dynamic response of a 28-inch-diameter ramjet engine was investigated for flight Mach numbers of...
Performance of four 16-inch-diameter ram-jet units was determined at free-stream Mach numbers of 0.4...
Free-flight performance of five 16-inch-diameter ram-jet units was determined over range of free-str...
Results obtained with three different burner configurations in a connected-pipe investigation of a 1...
A J34 turbojet engine was investigated at free-stream Mach numbers of 0.12 and 1.6 to 2.0 to determi...