Add to ORKGEffects of turbojet engine unstart on engine operation and characteristics of stall propagation through compressor and inlet syste
A J34 turbojet engine was investigated at free-stream Mach numbers of 0.12 and 1.6 to 2.0 to determi...
Effect of circumferential, radial, and combined pressure distortions on stall margin of J-85 engin
The throat of a Mach 2.5 inlet that was attached to a turbojet engine was fitted with a poppet-valve...
Steady-state interactions between turbojet engine and axisymmetric inlet with induced distortion
One of the propulsion system concepts to be considered for the High-Speed Civil Transport (HSCT) is ...
A two-dimensional inlet was alternately mated to a coldpipe plug assembly and a J85-GE-13 turbojet e...
Performance of turbojet in combination with external-internal-compression inlet at supersonic spee
An axisymmetric mixed-compression supersonic inlet and a single-spool turbojet engine were dynamical...
The paper explains how to analyse possible disturbances in the intake air stream and their impact on...
For a Mach number range from 1.6 to 2.0 and angles of attack from 0 to 9 degrees the occurrence of s...
Increased guide-vane turning resulted in poorer overall performance, the decrease being greatest at ...
Interaction of nacelle-mounted supersonic propulsion system with simulated wing boundary laye
Data are presented to show the response of an uncontrolled inlet to afterburner lightoff disturbance...
Wind tunnel tests for instantaneous and dynamic analysis of effects of time-variant distortions prod...
Performance tests of wind tunnel model inlet for bleed system back pressure and porous area effect o...
A J34 turbojet engine was investigated at free-stream Mach numbers of 0.12 and 1.6 to 2.0 to determi...
Effect of circumferential, radial, and combined pressure distortions on stall margin of J-85 engin
The throat of a Mach 2.5 inlet that was attached to a turbojet engine was fitted with a poppet-valve...
Steady-state interactions between turbojet engine and axisymmetric inlet with induced distortion
One of the propulsion system concepts to be considered for the High-Speed Civil Transport (HSCT) is ...
A two-dimensional inlet was alternately mated to a coldpipe plug assembly and a J85-GE-13 turbojet e...
Performance of turbojet in combination with external-internal-compression inlet at supersonic spee
An axisymmetric mixed-compression supersonic inlet and a single-spool turbojet engine were dynamical...
The paper explains how to analyse possible disturbances in the intake air stream and their impact on...
For a Mach number range from 1.6 to 2.0 and angles of attack from 0 to 9 degrees the occurrence of s...
Increased guide-vane turning resulted in poorer overall performance, the decrease being greatest at ...
Interaction of nacelle-mounted supersonic propulsion system with simulated wing boundary laye
Data are presented to show the response of an uncontrolled inlet to afterburner lightoff disturbance...
Wind tunnel tests for instantaneous and dynamic analysis of effects of time-variant distortions prod...
Performance tests of wind tunnel model inlet for bleed system back pressure and porous area effect o...
A J34 turbojet engine was investigated at free-stream Mach numbers of 0.12 and 1.6 to 2.0 to determi...
Effect of circumferential, radial, and combined pressure distortions on stall margin of J-85 engin
The throat of a Mach 2.5 inlet that was attached to a turbojet engine was fitted with a poppet-valve...