Flaperon modification effect on jet-flap interaction noise reduction for nozzles

13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference)

Volumn , Issue , 2007, Pages

  Mengle, Vinod G ^a   Stoker, Robert W ^a   Brusniak, Leon ^a   Elkoby, Ronen ^a   Thomas, Russell H ^b  

^a BOEING COMPANY   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COAXIAL NOZZLES; ENGINE CONFIGURATION; FAR-FIELD NOISE; MICROPHONE ARRAYS; MODIFICATION EFFECT; PARAMETRIC VARIATION; SOURCE DIAGNOSTICS; VORTEX GENERATORS;

ACOUSTIC NOISE; ENGINES; MICROPHONES; NOISE ABATEMENT; NOZZLES; TAKEOFF;

AEROACOUSTICS;

EID: 84884759613     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

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9. Mengle, V. G., Elkoby, R., Brusniak, L. and Thomas, R., "Reducing Propulsion Airframe Aeroacoustic Interactions with Uniquely Tailored Chevrons: 2. Installed Nozzles, " AIAA Paper 2006-2434, 2006.
10. Mengle, V. G., Brusniak, L., Elkoby, R., and Thomas, R., "Reducing Propulsion Airframe Aeroacoustic Interactions with Uniquely Tailored Chevrons: 3. Jet-Flap Interaction, " AIAA Paper 2006-2435, 2006.
11. Whitford, R., Design for Air Combat, Janes Publishing Co. Ltd., UK, 1987, pp. 108-109.
12. Massey, S. J, Elmiligui, A.A., Hunter, C.A., Thomas, R.H., Pao, S.P. and Mengle, V.G., "Computational Analysis of a Chevron Nozzle Uniquely Tailored for Propulsion Airframe Aeroacoustics, " AIAA Paper 2006-2436, 2006.