Add to ORKGPresented at the AIAA 5th Aviation, Technology, Integration, and Operations Conference (ATIO), 26 - ...
A Mach number measured in the subsonic diffuser was used experimentally as the inlet control paramet...
A mixed compression inlet designed for supersonic cruise has very demanding requirements for high to...
The techniques of modern optimal control theory were applied to the design of a control system for a...
Supersonic inlet engine control using engine speed as primary variable for controlling normal shock ...
The propulsion control requirements of supersonic aircraft are presented. Integration of inlet, engi...
Inlet pressure recovery of supersonic aircraft could be improved using a near-isentropic inlet with ...
Numerical study on controlling dynamic properties of supersonic inlet using bypass blee
A stability valve system designed for a full-scale, flight, supersonic, mixed-compression inlet was ...
Investigation of the control parameters of an external-internal compression inlet indicates that the...
학위논문 (박사)-- 서울대학교 대학원 : 기계항공공학부, 2013. 2. 김종암.This thesis aims to development of anti-buzz system in...
A cross-coupled inlet-engine control system concept is presented for a supersonic propulsion system ...
Inlet operating requirements are compared with estimated inlet separation characteristics to identif...
Presented at the AIAA 5th Aviation, Technology, Integration, and Operations Conference (ATIO), 26 - ...
The results of an experimental investigation to increase the stable airflow range (without unstart) ...
Presented at the AIAA 5th Aviation, Technology, Integration, and Operations Conference (ATIO), 26 - ...
A Mach number measured in the subsonic diffuser was used experimentally as the inlet control paramet...
A mixed compression inlet designed for supersonic cruise has very demanding requirements for high to...
The techniques of modern optimal control theory were applied to the design of a control system for a...
Supersonic inlet engine control using engine speed as primary variable for controlling normal shock ...
The propulsion control requirements of supersonic aircraft are presented. Integration of inlet, engi...
Inlet pressure recovery of supersonic aircraft could be improved using a near-isentropic inlet with ...
Numerical study on controlling dynamic properties of supersonic inlet using bypass blee
A stability valve system designed for a full-scale, flight, supersonic, mixed-compression inlet was ...
Investigation of the control parameters of an external-internal compression inlet indicates that the...
학위논문 (박사)-- 서울대학교 대학원 : 기계항공공학부, 2013. 2. 김종암.This thesis aims to development of anti-buzz system in...
A cross-coupled inlet-engine control system concept is presented for a supersonic propulsion system ...
Inlet operating requirements are compared with estimated inlet separation characteristics to identif...
Presented at the AIAA 5th Aviation, Technology, Integration, and Operations Conference (ATIO), 26 - ...
The results of an experimental investigation to increase the stable airflow range (without unstart) ...
Presented at the AIAA 5th Aviation, Technology, Integration, and Operations Conference (ATIO), 26 - ...
A Mach number measured in the subsonic diffuser was used experimentally as the inlet control paramet...
A mixed compression inlet designed for supersonic cruise has very demanding requirements for high to...