Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76033/1/AIAA-1985-1214-300.pd
Numerical simulations of the compressible, 3-D non reacting flow in the engine inlet sectionof a con...
Numerical simulations of the compressible, 3-D non reacting flow in the engine inlet sectionof a con...
An analytical investigation is performed to study the unsteady response of a one-dimensional, non-li...
Unsteady flow through a two-dimensional supersonic inlet-diffuser, with a normal shock wave in the d...
This paper investigates the flow in a supersonic mixed compression air intake using numerical simul...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77051/1/AIAA-10045-786.pd
A series of numerical simulations are carried out to analyze a supersonic inlet buzz, which is an un...
A numerical study was performed to simulate the critical flow through a supersonic inlet. This flow ...
Numerical study on controlling dynamic properties of supersonic inlet using bypass blee
학위논문 (박사)-- 서울대학교 대학원 : 기계항공공학부, 2013. 2. 김종암.This thesis aims to development of anti-buzz system in...
The supersonic diffuser of a Mach 2.68 bifurcated, rectangular, mixed-compression inlet was analyzed...
A Computational Fluid Dynamic investigation was conducted on a variable geometry supersonic/subsonic...
This thesis concentrates on the improvement of the quality of shock-dominated flows in supersonic in...
A method for calculating the flow field in aircraft engine inlets is presented. The phenomena of inl...
Inlet pressure recovery of supersonic aircraft could be improved using a near-isentropic inlet with ...
Numerical simulations of the compressible, 3-D non reacting flow in the engine inlet sectionof a con...
Numerical simulations of the compressible, 3-D non reacting flow in the engine inlet sectionof a con...
An analytical investigation is performed to study the unsteady response of a one-dimensional, non-li...
Unsteady flow through a two-dimensional supersonic inlet-diffuser, with a normal shock wave in the d...
This paper investigates the flow in a supersonic mixed compression air intake using numerical simul...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77051/1/AIAA-10045-786.pd
A series of numerical simulations are carried out to analyze a supersonic inlet buzz, which is an un...
A numerical study was performed to simulate the critical flow through a supersonic inlet. This flow ...
Numerical study on controlling dynamic properties of supersonic inlet using bypass blee
학위논문 (박사)-- 서울대학교 대학원 : 기계항공공학부, 2013. 2. 김종암.This thesis aims to development of anti-buzz system in...
The supersonic diffuser of a Mach 2.68 bifurcated, rectangular, mixed-compression inlet was analyzed...
A Computational Fluid Dynamic investigation was conducted on a variable geometry supersonic/subsonic...
This thesis concentrates on the improvement of the quality of shock-dominated flows in supersonic in...
A method for calculating the flow field in aircraft engine inlets is presented. The phenomena of inl...
Inlet pressure recovery of supersonic aircraft could be improved using a near-isentropic inlet with ...
Numerical simulations of the compressible, 3-D non reacting flow in the engine inlet sectionof a con...
Numerical simulations of the compressible, 3-D non reacting flow in the engine inlet sectionof a con...
An analytical investigation is performed to study the unsteady response of a one-dimensional, non-li...
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