Application of triple-deck theory to the prediction of glaze ice roughness formation on an airfoil leading edge

Computers and Fluids

Volumn 31, Issue 8, 2002, Pages 977-1014

  Tsao, J C ^a,b   Rothmayer, A P ^a  

^a IOWA STATE UNIVERSITY   (United States)

^b OHIO AEROSPACE INSTITUTE   (United States)

Author keywords

Aircraft icing; Free boundary value problem; Ice roughness formation; Interaction and instability of flows with phase change; Triple deck theory

Indexed keywords

COMPUTER SIMULATION; ICE; INTERFACES (MATERIALS); STABILIZATION; SURFACE ROUGHNESS; SURFACE TENSION; THERMOMECHANICAL TREATMENT; THIN FILMS;

AIRFOIL LEADING EDGE; GLAZE ICE ROUGHNESS FORMATION;

FLUID MECHANICS;

AIRCRAFT; COMPUTATIONAL FLUID DYNAMICS; ICE; ICING; INSTABILITY; PHASE CHANGE;

EID: 0036646755     PISSN: 00457930     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0045-7930(01)00050-0     Document Type: Article

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