-
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
-
-
33845638259
-
The Quiet Technology Demonstrator Program: Flight Validation of Airplane Noise-Reduction Concepts
-
AIAA-2006-2720, Cambridge, Massachusetts, USA, May
-
Herkes, W., Olsen, R., and Uellenberg, S. "The Quiet Technology Demonstrator Program: Flight Validation of Airplane Noise-Reduction Concepts, " 12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference), AIAA-2006-2720, Cambridge, Massachusetts, USA, May 2006.
-
(2006)
12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference)
-
-
Herkes, W.1
Olsen, R.2
Uellenberg, S.3
-
3
-
-
84884776531
-
The Quiet Technology Demonstrator Program: Static Test of an Acoustically Smooth Inlet
-
AIAA-2007-3671, Rome, Italy, May
-
Callender, B., Janardan, B., Premo, J., Uellenberg, S., Kwan, H., and Abeysinghe, A. "The Quiet Technology Demonstrator Program: Static Test of an Acoustically Smooth Inlet", 13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference), AIAA-2007-3671, Rome, Italy, May 2007.
-
(2007)
13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference)
-
-
Callender, B.1
Janardan, B.2
Premo, J.3
Uellenberg, S.4
Kwan, H.5
Abeysinghe, A.6
-
4
-
-
78249239741
-
Prediction of Inlet Splice Effects from the QTD2 Static Test
-
AIAA-2007-3544, Rome, Italy, May
-
Premo, J., Breard, C., Lan, J., Chin, E., Abeysinghe, A., and Callender, B. "Prediction of Inlet Splice Effects from the QTD2 Static Test", 13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference), AIAA-2007-3544, Rome, Italy, May 2007.
-
(2007)
13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference)
-
-
Premo, J.1
Breard, C.2
Lan, J.3
Chin, E.4
Abeysinghe, A.5
Callender, B.6
-
5
-
-
84884740311
-
Phased Array Measurements of Full-Scale Engine Inlet Noise
-
AIAA-2007-3434, Rome, Italy, May
-
Lan, J., Premo, J., Zlavog, G., Martinez, M., and Callender, B. "Phased Array Measurements of Full-Scale Engine Inlet Noise, " 13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference), AIAA-2007-3434, Rome, Italy, May 2007.
-
(2007)
13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference)
-
-
Lan, J.1
Premo, J.2
Zlavog, G.3
Martinez, M.4
Callender, B.5
-
6
-
-
84884791163
-
Phased Array Measurements of Full-Scale Engine Exhaust Noise
-
AIAA-2007-3612, Rome, Italy, May
-
Brusniak, L., Underbrink, J., Nesbitt, E., Lynch, D., and Martinez, M. "Phased Array Measurements of Full-Scale Engine Exhaust Noise", 13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference), AIAA-2007-3612, Rome, Italy, May 2007.
-
(2007)
13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference)
-
-
Brusniak, L.1
Underbrink, J.2
Nesbitt, E.3
Lynch, D.4
Martinez, M.5
-
7
-
-
85087594405
-
Effects of Chevrons on Engine Jet Noise Structure
-
AIAA-2007-3597, Rome, Italy, May
-
Nesbitt, E., Brusniak, L., Underbrink, J., Lynch, D., Martinez, M. "Effects of Chevrons on Engine Jet Noise Structure, " 13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference), AIAA-2007-3597, Rome, Italy, May 2007.
-
(2007)
13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference)
-
-
Nesbitt, E.1
Brusniak, L.2
Underbrink, J.3
Lynch, D.4
Martinez, M.5
-
8
-
-
84884740938
-
Shape Memory Alloy Based Morphing Chevrons: Full Scale Static Engine Test
-
AIAA-2007-3438, Rome, Italy, May
-
Calkins, F. and Mabe, J. "Shape Memory Alloy Based Morphing Chevrons: Full Scale Static Engine Test, " 13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference), AIAA-2007-3438, Rome, Italy, May 2007.
-
(2007)
13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference)
-
-
Calkins, F.1
Mabe, J.2
-
9
-
-
33845670830
-
Quiet Technology Demonstrator 2 Intake Liner Design and Validation
-
AIAA-2006-2458, Cambridge, Massachusetts, USA, May
-
th AIAA Aeroacoustics Conference), AIAA-2006-2458, Cambridge, Massachusetts, USA, 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
-
10
-
-
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
-
11
-
-
33845628095
-
Reducing Propulsion Airframe Aeroacoustic Interactions with Uniquely Tailored Chevrons: 1. Isolated Nozzles
-
AIAA-2006-2467, Cambridge, Massachusetts, USA, May
-
th AIAA Aeroacoustics Conference), AIAA-2006-2467, Cambridge, Massachusetts, USA, May 2006.
-
(2006)
th AIAA Aeroacoustics Conference)
-
-
Mengle, V.1
Elkoby, R.2
Brusniak, L.3
Thomas, R.4
-
12
-
-
33845796083
-
Reducing Propulsion Airframe Aeroacoustic Interactions with Uniquely Tailored Chevrons: 2. Installed Nozzles
-
AIAA-2006-2434, Cambridge, Massachusetts, USA, May
-
th AIAA Aeroacoustics Conference), AIAA-2006-2434, Cambridge, Massachusetts, USA, May 2006.
-
(2006)
th AIAA Aeroacoustics Conference)
-
-
Mengle, V.1
Elkoby, R.2
Brusniak, L.3
Thomas, R.4
-
13
-
-
33845773855
-
Flight Test Results for Uniquely Tailored Propulsion Airframe Aeroacoustic Chevrons: Community Noise
-
AIAA-2006-2438, Cambridge, Massachusetts, USA, May
-
th AIAA Aeroacoustics Conference), AIAA-2006-2438, Cambridge, Massachusetts, USA, May 2006.
-
(2006)
th AIAA Aeroacoustics Conference)
-
-
Nesbitt, E.1
Mengle, V.2
Czech, M.3
Callender, B.4
Thomas, R.5
-
14
-
-
33845791015
-
Effect of Uniform Chevrons on Cruise Shockcell Noise
-
AIAA-2006-2440, Cambridge, Massachusetts, USA, May
-
h AIAA Aeroacoustics Conference), AIAA-2006-2440, Cambridge, Massachusetts, USA, May 2006.
-
(2006)
h AIAA Aeroacoustics Conference)
-
-
Bultemeier, E.1
Ganz, U.2
Nesbitt, E.3
Premo, J.4
-
15
-
-
33845756270
-
Flight Test Results for Uniquely Tailored Propulsion Airframe Aeroacoustic Chevrons: Shockcell Noise
-
AIAA-2006-2439, Cambridge, Massachusetts, USA, May
-
th AIAA Aeroacoustics Conference), AIAA-2006-2439, Cambridge, Massachusetts, USA, May 2006.
-
(2006)
th AIAA Aeroacoustics Conference)
-
-
Mengle, V.1
Ganz, U.2
Nesbitt, E.3
Bultemeier, E.4
Thomas, R.5
-
16
-
-
33845672156
-
Variable Geometry Chevrons for Jet Noise Reduction
-
AIAA-2006-2546, Cambridge, Massachusetts, USA, May
-
th AIAA Aeroacoustics Conference), AIAA-2006-2546, Cambridge, Massachusetts, USA, May 2006.
-
(2006)
th AIAA Aeroacoustics Conference)
-
-
Calkins, F.1
Butler, G.2
Mabe, J.3
-
17
-
-
34147205259
-
Boeing's Variable Geometry Chevron: Morphing Aerostructure for Jet Noise reduction
-
AIAA-2006-2142, Newport, Rhode Island, USA, May
-
th AIAA Adaptive Structures Conference, AIAA-2006-2142, Newport, Rhode Island, USA, May 2006.
-
(2006)
th AIAA Adaptive Structures Conference
-
-
Mabe, J.1
Calkins, F.2
Butler, G.3
-
19
-
-
5244288213
-
A Compact Inflow Control Device for Simulating Flight Fan Noise
-
AIAA-1983-680, Atlanta, Georgia, USA, Apr
-
th AIAA Aeroacoustics Conference, AIAA-1983-680, Atlanta, Georgia, USA, Apr 1983.
-
(1983)
th AIAA Aeroacoustics Conference
-
-
Homyak, L.1
McArdle, J.2
Heidelberg, L.3
-
20
-
-
85003248729
-
Evaluation of Two Inflow Control Devices for Flight Simulation of Fan Noise Using a JT15D Engine
-
AIAA-1979-654, Seattle Washington, USA, March
-
th AIAA Aeroacoustics Conference, AIAA-1979-654, Seattle Washington, USA, March 1979.
-
(1979)
th AIAA Aeroacoustics Conference
-
-
Jones, W.1
McArdle, J.2
Homyak, L.3
-
21
-
-
56249129615
-
-
Society of Automotive Engineers, Inc. Aerospace Recommended Practice, SAE ARP 866A, issued August 1964, revised March
-
Society of Automotive Engineers, Inc. Aerospace Recommended Practice, SAE ARP 866A, "Standard Values of Atmospheric Absorption as a Function of Temperature and Humidity, " issued August 1964, revised March 1975.
-
(1975)
Standard Values of Atmospheric Absorption as a Function of Temperature and Humidity
-
-
-
22
-
-
84977085534
-
Phased Arrays for Aeroacoustic Testing-Theoretical Development
-
AIAA-1996-1713, State College Pennsylvania, USA, May
-
nd AIAA/CEAS Aeroacoustics Conference, AIAA-1996-1713, State College Pennsylvania, USA, May 1996.
-
(1996)
nd AIAA/CEAS Aeroacoustics Conference
-
-
Mosher, M.1
-
23
-
-
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
-
24
-
-
84896875791
-
Inlet Mode Measurements with an Inflow Control Device Microphone Array
-
AIAA2002-2563, Breckenridge, Colorado, USA, June
-
rd AIAA Aeroacoustics Conference), AIAA2002-2563, Breckenridge, Colorado, USA, June 2002.
-
(2002)
rd AIAA Aeroacoustics Conference)
-
-
Lan, J.1
Premo, J.2
Sutliff, D.3
|