Add to ORKGRestart and high response terminal shock control for axisymmetric mixed-compression inlet with internal contractio
The results of an experimental investigation to increase the stable airflow range of a super sonic m...
A cross-coupled inlet-engine control system concept is presented for a supersonic propulsion system ...
Dynamic response of supersonic mixed compression inlet coupled to cold pipe or turbojet engin
Results of experimental tests conducted on a supersonic, mixed-compression, axisymmetric inlet are p...
Shock and restart control systems with bypass doors and pressure transducers for mixed compression i...
Results of experimental tests conducted on a supersonic, mixed compression, axisymmetric inlet are p...
Digital computer control of a mixed-compression inlet is discussed. The inlet was terminated with a ...
Experimental results of terminal shock and restart control system tests of a two-dimensional, twin-d...
Investigation of the control parameters of an external-internal compression inlet indicates that the...
Wind tunnel tests of mixed-compression axisymmetric inlet system to determine bleed mass flow ratio,...
Supersonic inlet engine control using engine speed as primary variable for controlling normal shock ...
Normal shock control systems for supersonic mixed compression inlet using feedback loop
Experimental and analytical investigation of dynamic response of supersonic mixed-compression inle
Design and performance testing of large scale mixed compression axisymmetric inlet at transonic and ...
A digitally implemented integrated inlet-engine control system was designed and tested on a mixed-co...
The results of an experimental investigation to increase the stable airflow range of a super sonic m...
A cross-coupled inlet-engine control system concept is presented for a supersonic propulsion system ...
Dynamic response of supersonic mixed compression inlet coupled to cold pipe or turbojet engin
Results of experimental tests conducted on a supersonic, mixed-compression, axisymmetric inlet are p...
Shock and restart control systems with bypass doors and pressure transducers for mixed compression i...
Results of experimental tests conducted on a supersonic, mixed compression, axisymmetric inlet are p...
Digital computer control of a mixed-compression inlet is discussed. The inlet was terminated with a ...
Experimental results of terminal shock and restart control system tests of a two-dimensional, twin-d...
Investigation of the control parameters of an external-internal compression inlet indicates that the...
Wind tunnel tests of mixed-compression axisymmetric inlet system to determine bleed mass flow ratio,...
Supersonic inlet engine control using engine speed as primary variable for controlling normal shock ...
Normal shock control systems for supersonic mixed compression inlet using feedback loop
Experimental and analytical investigation of dynamic response of supersonic mixed-compression inle
Design and performance testing of large scale mixed compression axisymmetric inlet at transonic and ...
A digitally implemented integrated inlet-engine control system was designed and tested on a mixed-co...
The results of an experimental investigation to increase the stable airflow range of a super sonic m...
A cross-coupled inlet-engine control system concept is presented for a supersonic propulsion system ...
Dynamic response of supersonic mixed compression inlet coupled to cold pipe or turbojet engin