Boundary layer development in axial compressors and turbines part 4 of 4: computations & analyses

American Society of Mechanical Engineers (Paper)

Volumn , Issue , 1995, Pages

  Halstead, David E ^a   Wisler, David C ^a   Okiishi, Theodore H ^a   Walker, Gregory J ^a   Hodson, Howard P ^a   Shin, Hyoun Woo ^a  

^a GE AVIATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; CODES (SYMBOLS); COMPRESSORS; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; NAVIER STOKES EQUATIONS; NUMERICAL ANALYSIS; REYNOLDS NUMBER; TURBINES; TURBOMACHINE BLADES; TURBULENCE; DIFFUSION; EQUIPMENT TESTING; PRESSURE; PROBES; WAKES;

BOUNDARY LAYER CODES; PREDICTIVE CODES; HOT WIRE PROBES; LOW PRESSURE TURBINES; PRESSURE GRADIENT;

BOUNDARY LAYERS;

EID: 0029228434     PISSN: 04021215     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (0)