Control of shock-wave/boundary-layer interactions with passive blowing and bleeding

33rd Joint Propulsion Conference and Exhibit

Volumn , Issue , 1997, Pages

  Lin, Y L ^a   Rimlinger, M J ^a   Shih, T I P ^a   Willis, B P ^b  

^a CARNEGIE MELLON UNIVERSITY   (United States)

^b NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FINITE VOLUME METHOD; FLOW OF FLUIDS; PROPULSION; REYNOLDS NUMBER; SHOCK WAVES;

ALTERNATING DIRECTION IMPLICIT SCHEMES; COMPRESSIBLE NAVIER-STOKES; CONSERVATION EQUATIONS; ENSEMBLE-AVERAGED; FLUX DIFFERENCE SPLITTING; LOW REYNOLDS NUMBER; PASSIVE DEVICES; PRESSURE DIFFERENCES;

NAVIER STOKES EQUATIONS;

EID: 84962910696     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (25)

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