Non-Gaussian analysis of turbulent boundary layer fluctuating pressure on aircraft skin panels

Journal of Aircraft

Volumn 43, Issue 6, 2006, Pages 1662-1675

  Steinwolf, Alexander ^a,c   Rizzi, Stephen A ^b,d,e  

^a UNIVERSITY OF AUCKLAND   (New Zealand)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c Department of Mechanical Engineering ^*  (New Zealand)

^d Structural Acoustics Branch   (United States)

^e AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; MATHEMATICAL MODELS; POLYNOMIAL APPROXIMATION; PRESSURE MEASUREMENT; PROBABILITY DENSITY FUNCTION; STRUCTURAL PANELS;

AIRCRAFT SKIN PANELS; FLUCTUATING PRESSURE; NON GAUSSIAN ANALYSIS; SUPERSONIC TRANSPORT AIRCRAFT;

AIRCRAFT PARTS AND EQUIPMENT;

EID: 33846104196     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.18294     Document Type: Article

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