Explore: Engine Noise
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AI-Generated Overview About “engine-noise”:
Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Improved NASA-ANOPP noise prediction computer code for advanced subsonic propulsion systems
By K. B. Kontos
“Improved NASA-ANOPP noise prediction computer code for advanced subsonic propulsion systems” Metadata:
- Title: ➤ Improved NASA-ANOPP noise prediction computer code for advanced subsonic propulsion systems
- Author: K. B. Kontos
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Technical Information Service [distributor - National Aeronautics and Space Administration
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Improved NASA-ANOPP noise prediction computer code for advanced subsonic propulsion systems” Subjects and Themes:
- Subjects: ➤ Engine inlets - Pressure reduction - Aircraft noise - Aerodynamic noise - Noise reduction - Noise prediction - Engine noise
Edition Identifiers:
- The Open Library ID: OL18111692M - OL17122758M - OL15479071M - OL17546956M
- Online Computer Library Center (OCLC) ID: 38860517
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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2Ground-recorded sonic boom signatures of F-18 aircraft in formation flight
By Catherine M. Bahm
“Ground-recorded sonic boom signatures of F-18 aircraft in formation flight” Metadata:
- Title: ➤ Ground-recorded sonic boom signatures of F-18 aircraft in formation flight
- Author: Catherine M. Bahm
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“Ground-recorded sonic boom signatures of F-18 aircraft in formation flight” Subjects and Themes:
- Subjects: ➤ Aircraft engines - Engine noise - F-18 aircraft - Flight conditions - Loudness - Noise measurement - Signatures - Sonic booms
Edition Identifiers:
- The Open Library ID: OL18087400M - OL17106542M - OL15424016M
- Online Computer Library Center (OCLC) ID: 35268007
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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3Quiet high-speed fan
By Lysbeth Lieber
“Quiet high-speed fan” Metadata:
- Title: Quiet high-speed fan
- Author: Lysbeth Lieber
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Quiet high-speed fan” Subjects and Themes:
- Subjects: Aeroacoustics - Noise prediction - Turbofans - Engine noise - Noise reduction
Edition Identifiers:
- The Open Library ID: OL17593522M - OL18121546M - OL15505214M
- Online Computer Library Center (OCLC) ID: 41132219
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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4The use of cowl camber and taper to reduce rotor/stator interaction noise
By R. Martinez
“The use of cowl camber and taper to reduce rotor/stator interaction noise” Metadata:
- Title: ➤ The use of cowl camber and taper to reduce rotor/stator interaction noise
- Author: R. Martinez
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“The use of cowl camber and taper to reduce rotor/stator interaction noise” Subjects and Themes:
- Subjects: ➤ Aircraft noise - Camber - Cowlings - Ducts - Engine noise - Noise reduction - Predictions - Tapering
Edition Identifiers:
- The Open Library ID: OL15409816M - OL17788741M
- Online Computer Library Center (OCLC) ID: 32802314
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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5Computation of noise radiation from turbofans
By M. Nallasamy
“Computation of noise radiation from turbofans” Metadata:
- Title: ➤ Computation of noise radiation from turbofans
- Author: M. Nallasamy
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, D.C.?] - [Springfield, Va
“Computation of noise radiation from turbofans” Subjects and Themes:
- Subjects: ➤ Turbofans - Far fields - Air ducts - Noise prediction (Aircraft) - Aerodynamic noise - Turbofan engines - Aeroacoustics - Engine noise - Jet aircraft noise - Finite element method
Edition Identifiers:
- The Open Library ID: OL17794640M - OL17684879M
- Online Computer Library Center (OCLC) ID: 34702918
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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6Noise impact of advanced high lift systems
By Kevin R. Elmer
“Noise impact of advanced high lift systems” Metadata:
- Title: ➤ Noise impact of advanced high lift systems
- Author: Kevin R. Elmer
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: [Springfield, Va - Hampton, Va
“Noise impact of advanced high lift systems” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Aerodynamic noise - Aircraft design - Engine noise - Jet aircraft noise - Lift - Noise reduction - Passenger aircraft - Subsonic speed
Edition Identifiers:
- The Open Library ID: OL15416073M - OL17791319M
- Online Computer Library Center (OCLC) ID: 33241385
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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7Coupling of low speed fan stator vane unsteady pressures to duct modes
By Daniel L. Sutliff
“Coupling of low speed fan stator vane unsteady pressures to duct modes” Metadata:
- Title: ➤ Coupling of low speed fan stator vane unsteady pressures to duct modes
- Author: Daniel L. Sutliff
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: ➤ Springfield, VA - [Cleveland, Ohio]
“Coupling of low speed fan stator vane unsteady pressures to duct modes” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Noise intensity - Pressure distribution - Predictions - Ducted fans - Aircraft noise - Rotor stator interactions - Engine noise - Green's functions
Edition Identifiers:
- The Open Library ID: OL15550581M - OL17584189M
- Online Computer Library Center (OCLC) ID: 42333114
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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8Large Engine Technology (LET) task XXXVII low-bypass ratio mixed turbofan engine subsonic jet noise reduction program test report
By Joseph R. Hauser
“Large Engine Technology (LET) task XXXVII low-bypass ratio mixed turbofan engine subsonic jet noise reduction program test report” Metadata:
- Title: ➤ Large Engine Technology (LET) task XXXVII low-bypass ratio mixed turbofan engine subsonic jet noise reduction program test report
- Author: Joseph R. Hauser
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2001
- Publish Location: ➤ [Cleveland, Ohio] - Hanover, MD
“Large Engine Technology (LET) task XXXVII low-bypass ratio mixed turbofan engine subsonic jet noise reduction program test report” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Bypass ratio - Engine noise - Jet aircraft noise - Noise reduction - Subsonic flow
Edition Identifiers:
- The Open Library ID: OL16031810M - OL17604935M
- Online Computer Library Center (OCLC) ID: 49946276
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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9Database of inlet and exhaust noise shielding for wedge-shaped airframe
By Carl H. Gerhold
“Database of inlet and exhaust noise shielding for wedge-shaped airframe” Metadata:
- Title: ➤ Database of inlet and exhaust noise shielding for wedge-shaped airframe
- Author: Carl H. Gerhold
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - Available from NASA Center for AeroSpace Information (CASI)
- Publish Date: 2001
- Publish Location: Hanover, MD - Hampton, Va
“Database of inlet and exhaust noise shielding for wedge-shaped airframe” Subjects and Themes:
- Subjects: ➤ Engine noise - Airframes - Blended-wing-body configurations - Noise measurement
Edition Identifiers:
- The Open Library ID: OL16028996M - OL17607368M
- Online Computer Library Center (OCLC) ID: 50743536
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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10Separate flow nozzle test status meeting
“Separate flow nozzle test status meeting” Metadata:
- Title: ➤ Separate flow nozzle test status meeting
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 2000
- Publish Location: [Washington, DC] - Hanover, MD
“Separate flow nozzle test status meeting” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Sonic nozzles - Exhaust nozzles - Engine noise - Jet aircraft noise - Acoustic nozzles
Edition Identifiers:
- The Open Library ID: OL14524905M
- Online Computer Library Center (OCLC) ID: 50769127
Access and General Info:
- First Year Published: 2000
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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11Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet
By Michael K. Ponton
“Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet” Metadata:
- Title: ➤ Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet
- Author: Michael K. Ponton
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: Hampton, Va - [Springfield, Va
“Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet” Subjects and Themes:
- Subjects: ➤ Exhaust gases - Aeroacoustics - Exhaust nozzles - Jet flow - Flow characteristics - Subsonic flow - Convergent nozzles - High Reynolds number - Engine noise - Pressure oscillations
Edition Identifiers:
- The Open Library ID: OL15550628M
Author's Alternative Names:
"Nichael K. Ponton"Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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12Current wind tunnel capability and planned improvements at Lewis Research Center
By David N. Bowditch
“Current wind tunnel capability and planned improvements at Lewis Research Center” Metadata:
- Title: ➤ Current wind tunnel capability and planned improvements at Lewis Research Center
- Author: David N. Bowditch
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1986
- Publish Location: [Cleveland, Ohio
“Current wind tunnel capability and planned improvements at Lewis Research Center” Subjects and Themes:
- Subjects: ➤ Aircraft noise - Anechoic chambers - Engine noise - Lewis Research Center - Mach number - Propulsion system performance - Propulsive efficiency - Simulation - Supersonic wind tunnels - Wind tunnel tests - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL17727145M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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13A fan concept to meet the 2017 noise goals
By James H. Dittmar
“A fan concept to meet the 2017 noise goals” Metadata:
- Title: ➤ A fan concept to meet the 2017 noise goals
- Author: James H. Dittmar
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1998
- Publish Location: ➤ Springfield, VA - [Cleveland, Ohio]
“A fan concept to meet the 2017 noise goals” Subjects and Themes:
- Subjects: Compressors - Aircraft noise - Engine noise - Noise reduction - Design analysis
Edition Identifiers:
- The Open Library ID: OL15542465M
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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14An assessment of propeller aircraft noise reduction technology
By F. Bruce Metzger
“An assessment of propeller aircraft noise reduction technology” Metadata:
- Title: ➤ An assessment of propeller aircraft noise reduction technology
- Author: F. Bruce Metzger
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: [Springfield, Va - Hampton, Va
“An assessment of propeller aircraft noise reduction technology” Subjects and Themes:
- Subjects: ➤ Far fields - Propeller noise - Propellers - Aircraft noise - Aircraft engines - Noise reduction - Aircraft design - Engine noise
Edition Identifiers:
- The Open Library ID: OL15419910M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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15The reduction of ducted fan engine noise via a boundary integral equation method
By J. Tweed
“The reduction of ducted fan engine noise via a boundary integral equation method” Metadata:
- Title: ➤ The reduction of ducted fan engine noise via a boundary integral equation method
- Author: J. Tweed
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Dept. of Mathematics & Statistics, College of Engineering and Technology, Old Dominion University
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - Norfolk, Va - [Washington, DC
“The reduction of ducted fan engine noise via a boundary integral equation method” Subjects and Themes:
- Subjects: Boundary integral method - Ducted fan engines - Engine noise - Noise reduction - Noise prediction
Edition Identifiers:
- The Open Library ID: OL15543867M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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16Fan noise prediction assessment
By Paul H. Bent
“Fan noise prediction assessment” Metadata:
- Title: ➤ Fan noise prediction assessment
- Author: Paul H. Bent
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: [Springfield, Va - Hampton, Va
“Fan noise prediction assessment” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Directivity - Engine inlets - Noise prediction (Aircraft) - Finite element method - Aerodynamic noise - Engine noise - Nacelles
Edition Identifiers:
- The Open Library ID: OL15423091M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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17Aeroacoustic characteristics of a rectangular multi-element supersonic jet mixer-ejector nozzle
By Ganesh Raman
“Aeroacoustic characteristics of a rectangular multi-element supersonic jet mixer-ejector nozzle” Metadata:
- Title: ➤ Aeroacoustic characteristics of a rectangular multi-element supersonic jet mixer-ejector nozzle
- Author: Ganesh Raman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Aeroacoustic characteristics of a rectangular multi-element supersonic jet mixer-ejector nozzle” Subjects and Themes:
- Subjects: ➤ Pressure distribution - Nozzle geometry - Jet aircraft noise - Aerodynamic characteristics - Aircraft engines - Thrust augmentation - Engine noise - Acoustic properties
Edition Identifiers:
- The Open Library ID: OL15504879M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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18Supersonic jet noise reductions predicted with increased jet spreading rate
By Milo D. Dahl
“Supersonic jet noise reductions predicted with increased jet spreading rate” Metadata:
- Title: ➤ Supersonic jet noise reductions predicted with increased jet spreading rate
- Author: Milo D. Dahl
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Supersonic jet noise reductions predicted with increased jet spreading rate” Subjects and Themes:
- Subjects: ➤ Axisymmetric flow - Aeroacoustics - Jet mixing flow - Mathematical models - Supersonic jet flow - Noise prediction (Aircraft) - Aerodynamic noise - Noise reduction - Engine noise - Jet aircraft noise
Edition Identifiers:
- The Open Library ID: OL15411414M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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19Advanced turboprop wing installation effects measured by unsteady blade pressure and noise
By Laurence J. Heidelberg
“Advanced turboprop wing installation effects measured by unsteady blade pressure and noise” Metadata:
- Title: ➤ Advanced turboprop wing installation effects measured by unsteady blade pressure and noise
- Author: Laurence J. Heidelberg
- Language: English
- Number of Pages: Median: 21
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1987
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Advanced turboprop wing installation effects measured by unsteady blade pressure and noise” Subjects and Themes:
- Subjects: ➤ Wings - Turboprop engines - Unsteady flow - Pressure distribution - Propellers - Airplanes - Installing - Engine noise - Compressor blades
Edition Identifiers:
- The Open Library ID: OL15410914M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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20TBIEM3D
By M. H. Dunn
“TBIEM3D” Metadata:
- Title: TBIEM3D
- Author: M. H. Dunn
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service [distributor
- Publish Date: 1997
- Publish Location: Hampton, Va - Springfield, Va
“TBIEM3D” Subjects and Themes:
- Subjects: Noise prediction - Computer programs - Ducted fan engines - Engine noise - Programming languages
Edition Identifiers:
- The Open Library ID: OL15491176M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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21Noise certification predictions for FJX-2-powered aircraft using analytic methods
By Jeffrey J. Berton
“Noise certification predictions for FJX-2-powered aircraft using analytic methods” Metadata:
- Title: ➤ Noise certification predictions for FJX-2-powered aircraft using analytic methods
- Author: Jeffrey J. Berton
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: ➤ [Cleveland, Ohio] - [Springfield, Va
“Noise certification predictions for FJX-2-powered aircraft using analytic methods” Subjects and Themes:
- Subjects: ➤ Noise prediction (Aircraft) - Turbofan engines - Certification - Engine noise - General aviation aircraft - Jet aircraft noise
Edition Identifiers:
- The Open Library ID: OL15548208M
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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22Recent developments in U.S. engine noise reduction research
By James Bridges
“Recent developments in U.S. engine noise reduction research” Metadata:
- Title: ➤ Recent developments in U.S. engine noise reduction research
- Author: James Bridges
- Language: English
- Publisher: ➤ Available from NASA Center for AeroSpace Information - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2001
- Publish Location: Cleveland, Ohio - Hanover MD
“Recent developments in U.S. engine noise reduction research” Subjects and Themes:
- Subjects: Engine noise - Jet aircraft noise - Noise reduction - Research
Edition Identifiers:
- The Open Library ID: OL16037044M
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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23Theory for broadband noise of rotor and stator cascades with inhomogeneous inflow turbulence including effects of lean and sweep
By Donald B. Hanson
“Theory for broadband noise of rotor and stator cascades with inhomogeneous inflow turbulence including effects of lean and sweep” Metadata:
- Title: ➤ Theory for broadband noise of rotor and stator cascades with inhomogeneous inflow turbulence including effects of lean and sweep
- Author: Donald B. Hanson
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2001
- Publish Location: ➤ [Cleveland, Ohio] - Hanover, MD
“Theory for broadband noise of rotor and stator cascades with inhomogeneous inflow turbulence including effects of lean and sweep” Subjects and Themes:
- Subjects: ➤ Noise prediction - Turbofan engines - Homogeneous turbulence - Rotors - Interactional aerodynamics - Stators - Engine noise - Cascade flow
Edition Identifiers:
- The Open Library ID: OL16025805M
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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24UHB engine fan broadband noise reduction study
By Philip R. Gliebe
“UHB engine fan broadband noise reduction study” Metadata:
- Title: ➤ UHB engine fan broadband noise reduction study
- Author: Philip R. Gliebe
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“UHB engine fan broadband noise reduction study” Subjects and Themes:
- Subjects: ➤ Fan blades - Noise reduction - Blade slap noise - Engine tests - Broadband - Flight simulators - Turbine wheels - Turbofan engines - Noise generators - Engine noise
Edition Identifiers:
- The Open Library ID: OL15414971M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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25Comparison of predicted low speed fan rotor/stator interaction modes to measured
By Daniel L. Sutliff
“Comparison of predicted low speed fan rotor/stator interaction modes to measured” Metadata:
- Title: ➤ Comparison of predicted low speed fan rotor/stator interaction modes to measured
- Author: Daniel L. Sutliff
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Washington, DC - [Springfield, Va
“Comparison of predicted low speed fan rotor/stator interaction modes to measured” Subjects and Themes:
- Subjects: ➤ Aircraft noise - Aeroacoustics - Noise reduction - Ducted fans - Rotors - Stators - Engine noise
Edition Identifiers:
- The Open Library ID: OL15482765M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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Downloads Are Not Available:
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26Anaylsis of interior noise ground and flight test data for advanced turboprop aircraft applications
By Myles Simpson
“Anaylsis of interior noise ground and flight test data for advanced turboprop aircraft applications” Metadata:
- Title: ➤ Anaylsis of interior noise ground and flight test data for advanced turboprop aircraft applications
- Author: Myles Simpson
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1991
- Publish Location: Hampton, Va - [Springfield, Va
“Anaylsis of interior noise ground and flight test data for advanced turboprop aircraft applications” Subjects and Themes:
- Subjects: ➤ Control systems design - Noise reduction - Aircraft compartments - Aircraft noise - Turboprop engines - Turboprop aircraft - Ground tests - Engine noise
Edition Identifiers:
- The Open Library ID: OL15405415M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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27Acoustic properties of a supersonic fan
By Arthur W. Goldstein
“Acoustic properties of a supersonic fan” Metadata:
- Title: ➤ Acoustic properties of a supersonic fan
- Author: Arthur W. Goldstein
- Number of Pages: Median: 11
- Publisher: AIAA
- Publish Date: 1971
- Publish Location: New York
“Acoustic properties of a supersonic fan” Subjects and Themes:
- Subjects: Fan blades - Engine noise - Turbofan engines
Edition Identifiers:
- The Open Library ID: OL20898510M
Access and General Info:
- First Year Published: 1971
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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28Transmission of plane waves through a blade row
By Norman George Ball
“Transmission of plane waves through a blade row” Metadata:
- Title: ➤ Transmission of plane waves through a blade row
- Author: Norman George Ball
- Publisher: ➤ Dept. of Aerospace Science and Engineering
- Publish Date: 1979
- Publish Location: [Downsview, Ont.]
“Transmission of plane waves through a blade row” Subjects and Themes:
- Subjects: Engine noise - Plane waves
Edition Identifiers:
- The Open Library ID: OL19988480M
Access and General Info:
- First Year Published: 1979
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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29Separate flow nozzle test status meeting
“Separate flow nozzle test status meeting” Metadata:
- Title: ➤ Separate flow nozzle test status meeting
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 2000
- Publish Location: [Washington, DC] - Hanover, MD
“Separate flow nozzle test status meeting” Subjects and Themes:
- Subjects: ➤ Jet aircraft noise - Engine noise - Acoustic nozzles - Aeroacoustics - Sonic nozzles - Exhaust nozzles
Edition Identifiers:
- The Open Library ID: OL17607436M
- Online Computer Library Center (OCLC) ID: 50769127
Access and General Info:
- First Year Published: 2000
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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