Design and evaluation of modifications to the NASA Langley flow impedance tube

Collection of Technical Papers - 10th AIAA/CEAS Aeroacoustics Conference

Volumn 1, Issue , 2004, Pages 451-463

  Jones, M G ^a,c   Watson, W R ^a,d   Parrott, T L ^a,c   Smith, C D ^b,e  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b Lockheed Martin Engineering and Sciences   (United States)

^c Structural Acoustics Branch   (United States)

^d Mail Stop 128 ^*  (United States)

^e Mail Stop 105 ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC PRESSURE; ACOUSTIC REACTANCE; IMPEDANCE TUBES; TEST LINERS;

ACOUSTIC WAVE PROPAGATION; AIRCRAFT; AVIATION; BOUNDARY LAYER FLOW; MICROPHONES; OPTIMIZATION; PRESSURE MEASUREMENT; TUBES (COMPONENTS);

ACOUSTIC IMPEDANCE;

EID: 19644373951     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)

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