Large-eddy simulation of supersonic flat-plate boundary layers using the monotonically integrated large-eddy simulation (MILES) technique

Journal of Fluids Engineering, Transactions of the ASME

Volumn 124, Issue 4, 2002, Pages 868-875

  Yan, H ^a   Knight, D ^a   Zheltovodov, A A ^b  

^a RUTGERS UNIVERSITY   (United States)

^b KHRISTIANOVICH INSTITUTE OF THEORETICAL AND APPLIED MECHANICS   (Russian Federation)

Author keywords

[No Author keywords available]

Indexed keywords

DIRECT NUMERICAL SIMULATION (DNS); ISOTHERMAL SUPERSONIC FLAT PLATE BOUNDARY LAYERS; LEADING-ORDER TRUNCATION ERRORS; MONOTONICALLY INTEGRATED LARGE-EDDY SIMULATION (MILES);

BOUNDARY LAYER FLOW; COMPUTER SIMULATION; ERROR ANALYSIS; FINITE VOLUME METHOD; FRICTION; HEAT TRANSFER; INTEGRATION; ISOTHERMS; LOW PASS FILTERS; NAVIER STOKES EQUATIONS; PRANDTL NUMBER; REYNOLDS NUMBER; TURBULENT FLOW;

SUPERSONIC FLOW;

EID: 10844230411     PISSN: 00982202     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1516578     Document Type: Article

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