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Volumn , Issue , 2007, Pages

Effects of chevrons on engine jet noise structure

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; ACOUSTIC NOISE MEASUREMENT; AVIATION; BALANCING; MIXING; NOISE ABATEMENT; TESTING;

EID: 85087594405     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-3597     Document Type: Conference Paper
Times cited : (13)

References (19)
  • 1
    • 33845638259 scopus 로고    scopus 로고
    • The Quiet Technology Demonstrator Program: Flight Validation of Airplane Noise-Reduction Concepts
    • Herkes, W., Olsen, R., and Uellenberg, "The Quiet Technology Demonstrator Program: Flight Validation of Airplane Noise-Reduction Concepts, " AIAA Paper 2006-2720, 2006.
    • (2006) AIAA Paper 2006-2720
    • Herkes, W.1    Olsen, R.2    Uellenberg3
  • 2
    • 33845756270 scopus 로고    scopus 로고
    • Flight Test Results for Uniquely Tailored Propulsion Airframe Aeroacoustic Chevrons: Shockcell Noise
    • Mengle, V., Ganz, U., Nesbitt, E., Bultemeier, E. and Thomas, R. H., "Flight Test Results for Uniquely Tailored Propulsion Airframe Aeroacoustic Chevrons: Shockcell Noise, " AIAA Paper 2006-2439, 2006.
    • (2006) AIAA Paper 2006-2439
    • Mengle, V.1    Ganz, U.2    Nesbitt, E.3    Bultemeier, E.4    Thomas, R.H.5
  • 3
    • 33845773855 scopus 로고    scopus 로고
    • Flight Test Results for Uniquely Tailored Propulsion-Airframe Aeroacoustic Chevrons: Community Noise
    • Nesbitt, E., Mengle, V., Czech, M., Callender, B and Thomas, R. H., "Flight Test Results for Uniquely Tailored Propulsion-Airframe Aeroacoustic Chevrons: Community Noise, " AIAA Paper 2006-2438, 2006.
    • (2006) AIAA Paper 2006-2438
    • Nesbitt, E.1    Mengle, V.2    Czech, M.3    Callender, B.4    Thomas, R.H.5
  • 4
    • 33845628095 scopus 로고    scopus 로고
    • Reducing Propulsion Airframe Aeroacoustic Interactions with Uniquely Tailored Chevrons: 1. Isolated Nozzles
    • Mengle, V. G., Elkoby, R., Brusniak, L. and Thomas, R. H., "Reducing Propulsion Airframe Aeroacoustic Interactions with Uniquely Tailored Chevrons: 1. Isolated Nozzles, " AIAA Paper 2006-2467, 2006.
    • (2006) AIAA Paper 2006-2467
    • Mengle, V.G.1    Elkoby, R.2    Brusniak, L.3    Thomas, R.H.4
  • 6
    • 0041974174 scopus 로고
    • Engine Noise Source Breakdown: Theory, Simulation and Results
    • October
    • Tester, B.J., and Fisher, M.J., "Engine Noise Source Breakdown: Theory, Simulation and Results, " AIAA-81-2040, October 1981.
    • (1981) AIAA-81-2040
    • Tester, B.J.1    Fisher, M.J.2
  • 9
    • 84885691242 scopus 로고
    • An Empirical Model for Prediction of Coaxial Jet Noise in Ambient Flow
    • Lu, H. Y. "An Empirical Model for Prediction of Coaxial Jet Noise in Ambient Flow", AIAA-86-1912, 1986
    • (1986) AIAA-86-1912
    • Lu, H.Y.1
  • 10
    • 84884750584 scopus 로고    scopus 로고
    • Gas Turbine Jet Exhaust Noise Prediction
    • SAE Standard aAp876E, February
    • SAE Standard aAp876E "Gas Turbine Jet Exhaust Noise Prediction", Rev E, February 2006
    • (2006) Rev E
  • 11
    • 33845635181 scopus 로고    scopus 로고
    • A Method to Account for Engine Noise Component Source Locations
    • Salikuddin, M., Stimpert, D., and Majjigi, R., "A Method to Account for Engine Noise Component Source Locations, " AIAA-2006-2554, 2006.
    • (2006) AIAA-2006-2554
    • Salikuddin, M.1    Stimpert, D.2    Majjigi, R.3
  • 12
  • 13
    • 33845757572 scopus 로고    scopus 로고
    • Reducing Propulsion Airframe Aeroacoustic Interactions with Uniquely' Tailored Chevrons: 3. Jet-Flap Interaction
    • Mengle, V., Brusniak, L., Elkoby, R. and Thomas, R. H. "Reducing Propulsion Airframe Aeroacoustic Interactions with Uniquely' Tailored Chevrons: 3. Jet-Flap Interaction, " AIAA-2006-2435, 2006.
    • (2006) AIAA-2006-2435
    • Mengle, V.1    Brusniak, L.2    Elkoby, R.3    Thomas, R.H.4
  • 17
    • 84982318792 scopus 로고    scopus 로고
    • An empirical prediction of inlet radiated broadband noise from full scale engines
    • Nesbitt, E., Ganz, U., Diamond, J and Kosanchik III, M. "An empirical prediction of inlet radiated broadband noise from full scale engines" AIAA paper 1998-470, 1998.
    • (1998) AIAA paper 1998-470
    • Nesbitt, E.1    Ganz, U.2    Diamond, J.3    Kosanchik III, M.4
  • 19
    • 33845606270 scopus 로고    scopus 로고
    • Potential Errors Introduced in the use of Static Engine Noise Data not Acquired in Geometric Farfield
    • Ahuja, K.; Milway, S; and Churney, A. "Potential Errors Introduced in the use of Static Engine Noise Data not Acquired in Geometric Farfield" AIAA-2006-2553, 2006.
    • (2006) AIAA-2006-2553
    • Ahuja, K.1    Milway, S.2    Churney, A.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.