Effects of inlet distortion on the flow field in a transonic compressor rotor

American Society of Mechanical Engineers (Paper)

Volumn , Issue , 1996, Pages

  Hah, Chunill ^a   Rabe, Douglas C ^a   Sullivan, Thomas J ^a   Wadia, Aspi R ^a  

^a NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ASPECT RATIO; BOUNDARY CONDITIONS; COMPRESSORS; INTEGRATION; NAVIER STOKES EQUATIONS; NUMERICAL ANALYSIS; PRESSURE MEASUREMENT; PRESSURE TRANSDUCERS; REYNOLDS NUMBER; TRANSONIC AERODYNAMICS; TRANSONIC FLOW; VISCOUS FLOW;

FLOW FIELD; INLET DISTORTION; INLET TOTAL PRESSURE; THREE DIMENSIONAL VISCOUS FLOW CALCULATIONS; TIME INTEGRATION;

ROTORS;

EID: 18844467948     PISSN: 04021215     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (32)