Role of turbulent prandtl numbers on heat flux at hypersonic mach numbers

AIAA Journal

Volumn 45, Issue 4, 2007, Pages 806-813

  Xiao, X ^a,c,d   Hassan, H A ^a,c,d   Edwards, J R ^a,c,d   Gaffney Jr , R L ^b,d,e  

^a NORTH CAROLINA STATE UNIVERSITY   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c Department of Mechanical and Aerospace Engineering ^*

^d AIAA   (United States)

^e Hypersonic Air Breathing Propulsion Branch

Author keywords

[No Author keywords available]

Indexed keywords

BEAT TRANSFER; DISSIPATION RATE; ENERGY EQUATION; HYPERSONIC MACH NUMBERS;

HEAT FLUX; MATHEMATICAL MODELS; NAVIER STOKES EQUATIONS; PRANDTL NUMBER; REYNOLDS NUMBER; TURBULENCE; TURBULENT FLOW;

MACH NUMBER;

EID: 34247527332     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.21447     Document Type: Article

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