SCOPUS 정보 검색 플랫폼 - 논문 보기

메뉴 건너뛰기

Collection of Technical Papers - 12th AIAA/CEAS Aeroacoustics Conference

Volumn 6, Issue , 2006, Pages 4096-4104

The quiet technology demonstrator program: Flight validation of airplane noise-reduction concepts

(3) Herkes, William H a,b Olsen, Ronald F a,b Uellenberg, Stefan a,c

a BOEING COMPANY (United States)

b Mail Code 67 ML

c Noise Engineering (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; AIRCRAFT ENGINES; CABINS (AIRCRAFT); INTAKE SYSTEMS; NOZZLES; PROJECT MANAGEMENT;

FLIGHT TESTS; QUIET TECHNOLOGY DEMONSTRATOR 2 (QTD2);

NOISE ABATEMENT;

EID: 33845638259 PISSN: None EISSN: None Source Type: Conference Proceeding
DOI: 10.2514/6.2006-2720 Document Type: Conference Paper

Times cited : (59)

References (16)

1
- 19644381896
- The joint rolls-royce/boeing quiet technology demonstrator programme
- AIAA-2004-2869, Manchester UK, May
- th AIAA/CEAS Aeroacoustics Conference, AIAA-2004-2869, Manchester UK, May 2004.
- (2004) th AIAA/CEAS Aeroacoustics Conference
- Bartlett, P.¹ Humphreys, N.² Phillipson, P.³ Lan, J.⁴ Nesbitt, E.⁵ Premo, J.⁶

2
- 78149440518
- QTD2 (Quiet technology demonstrator 2) intake design and validation
- AIAA-2006-2458, Cambridge MA, May
- th AIAA Aeroacoustics Conference), AIAA-2006-2458, Cambridge MA, May 2006.
- (2006) th AIAA Aeroacoustics Conference)
- Yu, J.¹ Nesbitt, E.² Chien, E.³ Uellenberg, S.⁴ Kwan, H.⁵ Premo, J.⁶ Ruiz, M.⁷ Czech, M.⁸

3
- 0004874505
- The noise from shock waves in supersonic jets
- AGARD CP-131, Brussels, Belgium
- Harper-Bourne, M. and Fisher, M. "The Noise from Shock Waves in Supersonic Jets," Proceedings of the AGARD Conference on Noise Mechanisms, AGARD CP-131, pp 1-13, Brussels, Belgium, 1973.
- (1973) Proceedings of the AGARD Conference on Noise Mechanisms , pp. 1-13
- Harper-Bourne, M.¹ Fisher, M.²

4
- 29244487569
- Acoustic and flow-field characteristics of shock-cell noise from dual flow nozzles
- AIAA-2005-2929, Monterey CA, May
- th AIAA/CEAS Aeroacoustics Conference, AIAA-2005-2929, Monterey CA, May 2005.
- (2005) th AIAA/CEAS Aeroacoustics Conference
- Bhat, T.¹ Ganz, U.² Guthrie, A.³

5
- 33845628095
- Reducing propulsion airframe aeroacoustic interactions with uniquely tailored chevrons: 1. Isolated nozzles
- AIAA-2006-2467, Cambridge MA, May
- th AIAA Aeroacoustics Conference), AIAA-2006-2467, Cambridge MA, May 2006.
- (2006) th AIAA Aeroacoustics Conference)
- Mengle, V.¹ Elkoby, R.² Brusniak, L.³ Thomas, R.⁴

6
- 33845796083
- Reducing propulsion airframe aeroacoustic interactions with uniquely tailored chevrons: 2. Installed nozzles
- AIAA-2006-2434, Cambridge MA, May
- th AIAA Aeroacoustics Conference), AIAA-2006-2434, Cambridge MA, May 2006.
- (2006) th AIAA Aeroacoustics Conference)
- Mengle, V.¹ Elkoby, R.² Brusniak, L.³ Thomas, R.⁴

7
- 33845757572
- Reducing propulsion airframe aeroacoustic interactions with uniquely tailored chevrons: 3. Jet-flap interaction
- AIAA-2006-2435, Cambridge MA, May
- th AIAA Aeroacoustics Conference), AIAA-2006-2435, Cambridge MA, May 2006.
- (2006) th AIAA Aeroacoustics Conference)
- Mengle, V.¹ Elkoby, R.² Brusniak, L.³ Thomas, R.⁴

8
- 33845672156
- Variable geometry chevrons for jet noise reduction
- AIAA-2006-2546, Cambridge MA, May
- th AIAA Aeroacoustics Conference), AIAA-2006-2546, Cambridge MA, May 2006.
- (2006) th AIAA Aeroacoustics Conference)
- Calkins, F.¹ Butler, G.² Mabe, J.³

9
- 84977085534
- Phased arrays for aeroacoustic testing - Theoretical development
- AIAA-1996-1713, State College PA, May
- nd AIAA/CEAS Aeroacoustics Conference, AIAA-1996-1713, State College PA, May 1996.
- (1996) nd AIAA/CEAS Aeroacoustics Conference
- Mosher, M.¹

10
- 19644365127
- Aeroacoustic phased array testing in low speed wind tunnels
- edited by Thomas J. Mueller, Springer Verlag, Berlin
- Underbrink, J. "Aeroacoustic Phased Array Testing in Low Speed Wind Tunnels," Aeroacoustic Measurements, edited by Thomas J. Mueller, pp. 98-217, Springer Verlag, Berlin, 2002.
- (2002) Aeroacoustic Measurements , pp. 98-217
- Underbrink, J.¹

11
- 33845606682
- Acoustic imaging of aircraft noise sources using large aperture phased arrays
- AIAA-2006-2715, Cambridge MA, May
- th AIAA Aeroacoustics Conference), AIAA-2006-2715, Cambridge MA, May 2006.
- (2006) th AIAA Aeroacoustics Conference)
- Brusniak, L.¹ Underbrink, J.² Stoker, R.³

12
- 33845763348
- Novel inflight noise analysis system
- AIAA-2006-2437, Cambridge MA, May
- th AIAA Aeroacoustics Conference), AIAA-2006-2437, Cambridge MA, May 2006.
- (2006) th AIAA Aeroacoustics Conference)
- Hutto, F.¹ Bultemeier, E.²

13
- 33845645835
- Acoustic source localization in aircraft interiors using microphone array technologies
- AIAA-2006-2714, Cambridge MA, May
- th AIAA Aeroacoustics Conference), AIAA-2006-2714, Cambridge MA, May 2006.
- (2006) th AIAA Aeroacoustics Conference)
- Sklanka, B.¹ Tuss, J.² Buerhrle, R.³ Klos, J.⁴ Williams, E.⁵ Valdivia, N.⁶

14
- 33845773855
- Flight test results for uniquely tailored propulsion airframe aeroacoustic chevrons: Community noise
- AIAA-2006-2438, Cambridge MA, May
- th AIAA Aeroacoustics Conference), AIAA-2006-2438, Cambridge MA, May 2006.
- (2006) th AIAA Aeroacoustics Conference)
- Nesbitt, E.¹ Mengle, V.² Czech, M.³ Callender, B.⁴ Thomas, R.⁵

15
- 33845791015
- Effect of uniform chevrons on cruise shockceU noise
- AIAA-2006-2440, Cambridge MA, May
- th AIAA Aeroacoustics Conference), AIAA-2006-2440, Cambridge MA, May 2006.
- (2006) th AIAA Aeroacoustics Conference)
- Bultemeier, E.¹ Ganz, U.² Nesbitt, E.³ Premo, J.⁴

16
- 33845756270
- Flight test results for uniquely tailored propulsion airframe aeroacoustic chevrons: Shockcell noise
- AIAA-2006-2439, Cambridge MA, May
- th AIAA Aeroacoustics Conference), AIAA-2006-2439, Cambridge MA, May 2006.
- (2006) th AIAA Aeroacoustics Conference)
- Mengle, V.¹ Ganz, U.² Nesbitt, E.³ Bultemeier, E.⁴ Thomas, R.⁵

* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.