-
1
-
-
84878482972
-
Aviation and the Environment - Managing the Challenge of Growth
-
Plenary presentation at the First NASA Fundamental Aeronautics Annual Meeting, New Orleans, LA, October 30, .
-
Burleson, C., "Aviation and the Environment - Managing the Challenge of Growth," Plenary presentation at the First NASA Fundamental Aeronautics Annual Meeting, New Orleans, LA, October 30, 2007.
-
(2007)
-
-
Burleson, C.1
-
2
-
-
84878503852
-
Challenges and Opportunities for Noise Reduction Through Advanced Aircraft Propulsion Airframe Integration and Configurations
-
presented at the 8th CEAS Workshop on Aeroacoustics of New Aircraft and Engine Configurations, Budapest, Hungary, Nov. 11-12 .
-
Hill, G.A. and Thomas, R.H., "Challenges and Opportunities for Noise Reduction Through Advanced Aircraft Propulsion Airframe Integration and Configurations," presented at the 8th CEAS Workshop on Aeroacoustics of New Aircraft and Engine Configurations, Budapest, Hungary, Nov. 11-12, 2004.
-
(2004)
-
-
Hill, G.A.1
Thomas, R.H.2
-
3
-
-
84864604678
-
Integration of Propulsion Airframe Aeroacoustic Technologies and Design Concepts for a Quiet Blended Wing Body Transport
-
AIAA Paper 2004-6306.
-
Hill, G.A., Brown, S.A., Geiselhart, K.A., and Burg, C.M., "Integration of Propulsion Airframe Aeroacoustic Technologies and Design Concepts for a Quiet Blended Wing Body Transport," AIAA Paper 2004-6306.
-
-
-
Hill, G.A.1
Brown, S.A.2
Geiselhart, K.A.3
Burg, C.M.4
-
4
-
-
78649590448
-
Subsonic Fixed Wing Project N+2 Noise Goal Summary
-
presentation at the NASA Acoustics Technical Working Group, December 4-5, Cleveland, OH.
-
Thomas, R.H., "Subsonic Fixed Wing Project N+2 Noise Goal Summary," presentation at the NASA Acoustics Technical Working Group, December 4-5, 2007, Cleveland, OH.
-
(2007)
-
-
Thomas, R.H.1
-
5
-
-
33845663178
-
Noise Scattering by the Blended Wing Body Airplane: Measurements and Prediction
-
AIAA Paper No. 2006-2474, presented at the 12th AIAA/CEAS Aeroacoustics Conference, Cambridge, MA, .
-
Reimann, C. A., Tinetti, A.F., and Dunn, M.H., "Noise Scattering by the Blended Wing Body Airplane: Measurements and Prediction," AIAA Paper No. 2006-2474, presented at the 12th AIAA/CEAS Aeroacoustics Conference, Cambridge, MA, 2006.
-
(2006)
-
-
Reimann, C.A.1
Tinetti, A.F.2
Dunn, M.H.3
-
6
-
-
84982318818
-
Inlet Noise Reduction By Shielding for the Blended Wing Body Airplane
-
AIAA Paper No. 99-1937, presented at the 5th AIAA/CEAS Aeroacoustics Conference, Seattle, WA, .
-
Clark, L.R. and Gerhold, C.H., "Inlet Noise Reduction By Shielding for the Blended Wing Body Airplane," AIAA Paper No. 99-1937, presented at the 5th AIAA/CEAS Aeroacoustics Conference, Seattle, WA, 1999.
-
(1999)
-
-
Clark, L.R.1
Gerhold, C.H.2
-
7
-
-
78649589918
-
Propulsion Airframe Aeroacoustic Integration Effects of a Hybrid Wing Body Aircraft Configuration
-
AIAA Paper No. 2010-3912, presented at the 16th AIAA/CEAS Aeroacoustics Conference, Stockholm, Sweden, June 7-9,
-
Czech, M., Thomas, R., and Elkoby, R., "Propulsion Airframe Aeroacoustic Integration Effects of a Hybrid Wing Body Aircraft Configuration," AIAA Paper No. 2010-3912, presented at the 16th AIAA/CEAS Aeroacoustics Conference, Stockholm, Sweden, June 7-9, 2010.
-
(2010)
-
-
Czech, M.1
Thomas, R.2
Elkoby, R.3
-
8
-
-
85088719474
-
Experimental Study of Acoustic Characteristics of Jets from Dual Flow Nozzles
-
AIAA Paper 2001-2183.
-
Bhat. T.R.S., "Experimental Study of Acoustic Characteristics of Jets from Dual Flow Nozzles." AIAA Paper 2001-2183, 2001.
-
(2001)
-
-
Bhat, T.R.S.1
-
9
-
-
19644400380
-
Jet Noise Reduction Technology Development at GE Aircraft Engines
-
ICAS Paper 842, presented at the International Council of the Aeronautical Sciences, Toronto, Canada, September, .
-
Martens, S., "Jet Noise Reduction Technology Development at GE Aircraft Engines." ICAS Paper 842, presented at the International Council of the Aeronautical Sciences, Toronto, Canada, September, 2002.
-
(2002)
-
-
Martens, S.1
-
10
-
-
19644397325
-
Jet-Pylon Interaction of High Bypass Ratio Separate Flow Nozzle Configurations
-
AIAA Paper No. 2004-2827, presented at the 10th AIAA/CEAS Aeroacoustics Conference, Manchester, United Kingdom, May 10-12, .
-
Thomas, R., and Kinzie, K., "Jet-Pylon Interaction of High Bypass Ratio Separate Flow Nozzle Configurations," AIAA Paper No. 2004-2827, presented at the 10th AIAA/CEAS Aeroacoustics Conference, Manchester, United Kingdom, May 10-12, 2004.
-
(2004)
-
-
Thomas, R.1
Kinzie, K.2
-
11
-
-
33745949548
-
Computational and Experimental Flow Field Analyses of Separate Flow Chevron Nozzles and Pylon Interaction
-
AIAA Paper 2003-3212, .
-
Massey, S., Thomas, R., Abdol-Hamid, K., Elmiligui, A.: "Computational and Experimental Flow Field Analyses of Separate Flow Chevron Nozzles and Pylon Interaction." AIAA Paper 2003-3212, 2003.
-
(2003)
-
-
Massey, S.1
Thomas, R.2
Abdol-hamid, K.3
Elmiligui, A.4
-
12
-
-
33845652389
-
Development of a Jet Noise Prediction Method for Installed Jet Configurations
-
AIAA Paper 2003-3169
-
Hunter. C., and Thomas, R., "Development of a Jet Noise Prediction Method for Installed Jet Configurations." AIAA Paper 2003-3169, 2003.
-
(2003)
-
-
Hunter, C.1
Thomas, R.2
-
13
-
-
77949916373
-
Computational Analysis of the Flow and Acoustic Effects of Jet-Pylon Interaction
-
AIAA Paper No. 2005-3083, May,
-
Hunter, C.A., Thomas, R.H., Abdol-Hamid, K.S., and Pao, S.P., Elmiligui, A.A., and Massey, S.J., "Computational Analysis of the Flow and Acoustic Effects of Jet-Pylon Interaction," AIAA Paper No. 2005-3083, May, 2005.
-
(2005)
-
-
Hunter, C.A.1
Thomas, R.H.2
Abdol-hamid, K.S.3
Pao, S.P.4
Elmiligui, A.A.5
Massey, S.J.6
-
14
-
-
33845773855
-
Flight Test Results for Uniquely Tailored Propulsion Airframe Aeroacoustic Chevrons: Community Noise
-
Nesbitt, E., Mengle, V., Czech, M., Callendar, B., and Thomas, R., "Flight Test Results for Uniquely Tailored Propulsion Airframe Aeroacoustic Chevrons: Community Noise," AIAA Paper 2006-2438, May, 2006.
-
(2006)
AIAA Paper 2006-2438, May,
-
-
Nesbitt, E.1
Mengle, V.2
Czech, M.3
Callendar, B.4
Thomas, R.5
-
15
-
-
33845628095
-
Reducing Propulsion Airframe Aeroacoustic Interactions with Uniquely Tailored Chevrons: Part 1. Isolated Nozzles
-
AIAA Paper No. 2006-2467, May,
-
Mengle, V., Elkoby, R., Brusniak, L., and Thomas, R., "Reducing Propulsion Airframe Aeroacoustic Interactions with Uniquely Tailored Chevrons: Part 1. Isolated Nozzles," AIAA Paper No. 2006-2467, May, 2006.
-
(2006)
-
-
Mengle, V.1
Elkoby, R.2
Brusniak, L.3
Thomas, R.4
-
16
-
-
33845742971
-
Computational Analysis of a Chevron Nozzle Uniquely Tailored for Propulsion Airframe Aeroacoustics
-
AIAA Paper No. 2006-2436, May,
-
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 No. 2006-2436, May, 2006.
-
(2006)
-
-
Massey, S.J.1
Elmiligui, A.A.2
Hunter, C.A.3
Thomas, R.H.4
Pao, S.P.5
Mengle, V.G.6
-
17
-
-
78649532413
-
Hybrid Wing Body Aircraft System Noise Assessment With Propulsion Airframe Aeroacoustic Experiments
-
AIAA Paper No. 2010-3913, presented at the 16th AIAA/CEAS Aeroacoustics Conference, Stockholm, Sweden, June 7-9,
-
Thomas, R.H., Burley, C.L., and Olson, E.D., "Hybrid Wing Body Aircraft System Noise Assessment With Propulsion Airframe Aeroacoustic Experiments," AIAA Paper No. 2010-3913, presented at the 16th AIAA/CEAS Aeroacoustics Conference, Stockholm, Sweden, June 7-9, 2010.
-
(2010)
-
-
Thomas, R.H.1
Burley, C.L.2
Olson, E.D.3
-
18
-
-
78249260134
-
Hybrid Wing Body Configuration System Studies
-
AIAA Paper No. 2009-931.
-
Nickol, C.L., and McCullers, L., "Hybrid Wing Body Configuration System Studies," AIAA Paper No. 2009-931.
-
-
-
Nickol, C.L.1
McCullers, L.2
-
19
-
-
84983155169
-
A Parabolic Approximation for Flow Effects on Sound Propagation in Nonuniform, Softwall, Ducts
-
AIAA Paper No. 99-1822, presented at the 5th AIAA/CEAS Aeroacoustics Conference, Seattle, WA,
-
Dougherty, R.P., "A Parabolic Approximation for Flow Effects on Sound Propagation in Nonuniform, Softwall, Ducts," AIAA Paper No. 99-1822, presented at the 5th AIAA/CEAS Aeroacoustics Conference, Seattle, WA, 1999.
-
(1999)
-
-
Dougherty, R.P.1
-
20
-
-
19944375128
-
Effects of Bifurcations on Aft-Fan Engine Nacelle Noise
-
AIAA Paper No. 2004-2988, presented at the 10th AIAA/CEAS Aeroacoustics Conference, Manchester, United Kingdom, May 10-12,
-
Nark, D.M., Farassat, F., Pope, S.D., and Vatsa, V., "Effects of Bifurcations on Aft-Fan Engine Nacelle Noise," AIAA Paper No. 2004-2988, presented at the 10th AIAA/CEAS Aeroacoustics Conference, Manchester, United Kingdom, May 10-12, 2004.
-
(2004)
-
-
Nark, D.M.1
Farassat, F.2
Pope, S.D.3
Vatsa, V.4
-
21
-
-
78149435062
-
An Analytical Assessment of NASA's N+1 Subsonic Fixed Wing Project Noise Goal
-
AIAA Paper No. 2009-3144, presented at the 15th AIAA/CEAS Aeroacoustics Conference, Miami, FL, May
-
Berton, J.J., Envia, E., and Burley, C.L., "An Analytical Assessment of NASA's N+1 Subsonic Fixed Wing Project Noise Goal," AIAA Paper No. 2009-3144, presented at the 15th AIAA/CEAS Aeroacoustics Conference, Miami, FL, May, 2009.
-
(2009)
-
-
Berton, J.J.1
Envia, E.2
Burley, C.L.3
-
22
-
-
0342604571
-
Aircraft Noise Prediction Program Theoretical Manual
-
NASA TM-83199
-
Zorumski, W. E., "Aircraft Noise Prediction Program Theoretical Manual," NASA TM-83199, 1982.
-
(1982)
-
-
Zorumski, W.E.1
-
23
-
-
0001254478
-
Noise Reduction by Screens
-
Maekawa, Z. "Noise Reduction by Screens," Applied Acoustics, Vol.1, 1968, pp. 157-173.
-
(1968)
Applied Acoustics
, vol.1
, pp. 157-173
-
-
Maekawa, Z.1
-
24
-
-
78249289992
-
Maggi-Rubinowicz Diffraction Correction for Ray-tracing Calculations of Engine Noise Shielding
-
AIAA 2008-3050, 14th AIAA/CEAS Aeroacoustics Conference. Vancouver, British Columbia Canada, May 5-7
-
Lummer, M., "Maggi-Rubinowicz Diffraction Correction for Ray-tracing Calculations of Engine Noise Shielding", AIAA 2008-3050, 14th AIAA/CEAS Aeroacoustics Conference. Vancouver, British Columbia Canada, May 5-7, 2008.
-
(2008)
-
-
Lummer, M.1
-
25
-
-
78249253362
-
Numerical Study of Noise Shielding by Airfram Structures
-
AIAA 2008-2999, 14th AIAA/CEAS Aeroacoustics Conference. Vancouver, British Columbia Canada, May 5-7
-
Huang, C., and Papamoschou, D., "Numerical Study of Noise Shielding by Airfram Structures", AIAA 2008-2999, 14th AIAA/CEAS Aeroacoustics Conference. Vancouver, British Columbia Canada, May 5-7, 2008.
-
(2008)
-
-
Huang, C.1
Papamoschou, D.2
-
26
-
-
78249250021
-
Application of Multipole Methods to the NASA Fast Scattering Code
-
AIAA 2008-2875, 14th AIAA/CEAS Aeroacoustics Conference. Vancouver, British Columbia Canada, May 5-
-
Dunn, M., and Tinetti, A., "Application of Multipole Methods to the NASA Fast Scattering Code", AIAA 2008-2875, 14th AIAA/CEAS Aeroacoustics Conference. Vancouver, British Columbia Canada, May 5-7, 2008.
-
(2008)
-
-
Dunn, M.1
Tinetti, A.2
-
27
-
-
77953217524
-
Acoustic Prediction Methodology and Test Validation for an Efficient Low Noise Hybrid Wing Body Subsonic Transport
-
presentation at the NASA Acoustics Technical Working Group Meeting, December 4-5, Cleveland, OH.
-
Kawai, R.T., "Acoustic Prediction Methodology and Test Validation for an Efficient Low Noise Hybrid Wing Body Subsonic Transport," presentation at the NASA Acoustics Technical Working Group Meeting, December 4-5, 2007, Cleveland, OH.
-
(2007)
-
-
Kawai, R.T.1
-
28
-
-
34250832150
-
Airframe Design for "Silent Aircraft"
-
AIAA Paper 2007-0453
-
Hileman, J.I., Spakovszky, Z.S., Drela, M., and Sargeant, M.A., "Airframe Design for "Silent Aircraft"," AIAA Paper 2007-0453, 2007.
-
(2007)
-
-
Hileman, J.I.1
Spakovszky, Z.S.2
Drela, M.3
Sargeant, M.A.4
-
29
-
-
78049387551
-
777 Airplane Characteristics for Airport Planning
-
777-200LR/300ER/777F Document D6-58329-2 (Revision D, August, 2009). , accessed April,
-
777 Airplane Characteristics for Airport Planning, 777-200LR/300ER/777F Document D6-58329-2 (Revision D, August, 2009). http://www.boeing.com/commercial/airports/plan_manuals.html, accessed April, 2010.
-
(2010)
-
-
-
30
-
-
84878498084
-
-
StartupBoeing - Boeing Passenger Airplanes, 777 (777-200/-200ER/-200LR/-300/-300ER) "Characteristics & Performance Summary.pdf", slide 7/11., accessed June,
-
StartupBoeing - Boeing Passenger Airplanes, 777 (777-200/-200ER/-200LR/-300/-300ER) "Characteristics & Performance Summary.pdf", slide 7/11.http://www.boeing.com/commercial/startup/pdf/77_perf.pdf, accessed June, 2010.
-
(2010)
-
-
-
31
-
-
78549295948
-
Hybrid Wing Body Configuration System Studies
-
AIAA 2009-931, January
-
Nickol, C.L, McCullers, L.A., "Hybrid Wing Body Configuration System Studies", AIAA 2009-931, January 2009.
-
(2009)
-
-
Nickol, C.L.1
McCullers, L.A.2
-
32
-
-
78549231995
-
Airframe Development for the Hybrid Wing Body Aircraft
-
AIAA 2009-932, January,
-
Velicki, A., Thrash, P., Jegley, D., "Airframe Development for the Hybrid Wing Body Aircraft", AIAA 2009-932, January, 2009.
-
(2009)
-
-
Velicki, A.1
Thrash, P.2
Jegley, D.3
-
33
-
-
0024640732
-
Gust Load Alleviation of a Transport-Type Wing: Test and Analysis
-
AIAA Journal of Aircraft
-
Matsuzaki, Y., et. al., "Gust Load Alleviation of a Transport-Type Wing: Test and Analysis", AIAA Journal of Aircraft, Vol. 26, No. 4, 1987.
-
(1987)
, vol.26
, Issue.4
-
-
Matsuzaki, Y.1
-
34
-
-
34547541826
-
A Systems MDO Approach for an Unmanned Aerial Vehicle
-
AIAA 2007-1877, April,
-
Hunten, K., et. al., "A Systems MDO Approach for an Unmanned Aerial Vehicle", AIAA 2007-1877, April, 2007.
-
(2007)
-
-
Hunten, K.1
-
35
-
-
0003436658
-
Overview of Laminar Flow Control
-
NASA/TP-1998-208705, October,
-
Joslin, R.D., "Overview of Laminar Flow Control", NASA/TP-1998-208705, October, 1998.
-
(1998)
-
-
Joslin, R.D.1
-
36
-
-
85001975627
-
Riblet Drag Reduction at Flight Conditions
-
AIAA 1988-2554, June,
-
Walsh, M.J., Sellers, W.L., and, McGinley, C.B., "Riblet Drag Reduction at Flight Conditions", AIAA 1988-2554, June, 1988.
-
(1988)
-
-
Walsh, M.J.1
Sellers, W.L.2
McGinley, C.B.3
-
37
-
-
84872392485
-
Optimization of Segmented Flaps for In-flight Transonic Performance Enhancement
-
AIAA 1997-0516, January,
-
Siclari, M.J., et. al., "Optimization of Segmented Flaps for In-flight Transonic Performance Enhancement", AIAA 1997-0516, January, 1997.
-
(1997)
-
-
Siclari, M.J.1
-
38
-
-
68649090014
-
Subsystem Design and Integration for the More Electric Aircraft
-
AIAA 2007-4828, June,
-
Blanding, D., "Subsystem Design and Integration for the More Electric Aircraft", AIAA 2007-4828, June, 2007.
-
(2007)
-
-
Blanding, D.1
-
39
-
-
60049100778
-
Analysis of Solid Oxide Fuel Cell Systems for More-Electric Aircraft
-
Jan- Feb
-
Santarelli, M. Cabrera, M., Cali, M., 'Analysis of Solid Oxide Fuel Cell Systems for More-Electric Aircraft", AIAA Journal of Aircraft, Vol. 46, No. 1, Jan- Feb 2009.
-
(2009)
AIAA Journal of Aircraft
, vol.46
, Issue.1
-
-
Santarelli, M.1
Cabrera, M.2
Cali, M.3
-
40
-
-
34548728845
-
Solid Oxide Fuel Cell/Gas Turbine Hybrid Cycle Technology for Auxiliary Aerospace Power
-
NASA/TM- 2005-213586, April,
-
Steffen, C.J., Freeh, J.E., Larosiliere, L.M., "Solid Oxide Fuel Cell/Gas Turbine Hybrid Cycle Technology for Auxiliary Aerospace Power", NASA/TM- 2005-213586, April, 2005.
-
(2005)
-
-
Steffen, C.J.1
Freeh, J.E.2
Larosiliere, L.M.3
-
41
-
-
33947610840
-
Blended Wing Body Analysis and Design
-
AIAA 1997-2317, June,
-
Potsdam, M.A., Page, M.A., Liebeck, R.H., "Blended Wing Body Analysis and Design", AIAA 1997-2317, June, 1997.
-
(1997)
-
-
Potsdam, M.A.1
Page, M.A.2
Liebeck, R.H.3
-
42
-
-
84982319197
-
Blended-Wing-Body Subsonic Commercial Transport
-
AIAA 1998-0438, January,
-
Liebeck, R.H., Page, M.A., Rawdon, B.K., "Blended-Wing-Body Subsonic Commercial Transport", AIAA 1998-0438, January, 1998.
-
(1998)
-
-
Liebeck, R.H.1
Page, M.A.2
Rawdon, B.K.3
-
43
-
-
34250794515
-
Challenges in the Silent Aircraft Engine Design
-
AIAA 2007-454, January
-
Blanco, E.R., Hall, C.A., Crichton, D., "Challenges in the Silent Aircraft Engine Design", AIAA 2007-454, January, 2007.
-
(2007)
-
-
Blanco, E.R.1
Hall, C.A.2
Crichton, D.3
-
44
-
-
34250822933
-
Performance of a Boundary Layer Ingesting (BLI) Propulsion System
-
AIAA 2007-450, January,
-
Plas, A.P., et. al., 'Performance of a Boundary Layer Ingesting (BLI) Propulsion System", AIAA 2007-450, January, 2007.
-
(2007)
-
-
Plas, A.P.1
|