Boundary-layer transition under the effect of compressibility for the correlation Based Transition Model

46th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2008, Pages

  Kaynak, Ünver ^a   Gürdamar, Emre ^b  

^a TOBB UNIVERSITY OF ECONOMICS AND TECHNOLOGY   (Turkey)

^b MIDDLE EAST TECHNICAL UNIVERSITY   (Turkey)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER TRANSITIONS; BOUNDARY-LAYER TRANSITION; BYPASS TRANSITION; COMPRESSIBILITY EFFECTS; COMPRESSIBILITY FACTOR; EMPIRICAL CORRELATIONS; EXPERIMENTAL DATA; FLAT PLATE; FREESTREAM TURBULENCE; HIGH MACH NUMBER; LINEAR STABILITY THEORY; LOW MACH NUMBERS; NEW CORRELATIONS; NUMERICAL RESULTS; SUPERSONIC SPEED; TRANSITION MODEL; TRANSITION PREDICTION; TRANSITION REGIONS;

AEROSPACE ENGINEERING; BOUNDARY LAYERS; COMPRESSIBILITY; EXPERIMENTS; MACH NUMBER; SUPERSONIC AERODYNAMICS; TURBULENCE MODELS;

ATMOSPHERIC THERMODYNAMICS;

EID: 78149424660     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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