Inlet noise reduction by shielding for the blended-wing-body airplane

5th AIAA/CEAS Aeroacoustics Conference and Exhibit

Volumn , Issue , 1999, Pages 891-898

  Clark, Lorenzo R ^a   Gerhold, Carl H ^a  

^a NONE

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC FIELDS; ACOUSTICS; AEROACOUSTICS; AIRCRAFT ENGINES; ENGINES; FLOW CONTROL; MICROPHONES; NASA; NOISE ABATEMENT; SHIELDING;

BLENDED WING BODY; FREQUENCY RANGES; HIGH FREQUENCY HF; LOWER FREQUENCIES; MICROPHONE ARRAYS; NASA LANGLEY RESEARCH CENTER; RESEARCH FACILITIES; SHIELDING EFFICIENCY;

ACOUSTIC NOISE;

EID: 84982318818     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (2)

1. The Boeing Company, Long Beach, CA, “Blended-Wing-Body Technology Study”, Final Report No. CR AD-9405TR-3780, prepared for NASA-Langley Research Center under NAS1-20275, October 1997.
2. Hubbard, Harvey H.; and Manning, James C, “Aeroacoustic Research Facilities at NASA Langley Research Center”, NASA TM 84585, March 1983.