Explore: Nacelles
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AI-Generated Overview About “nacelles”:
Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Boundary-layer separation on isolated boattail nozzles
By William Kelly Abeyounis
“Boundary-layer separation on isolated boattail nozzles” Metadata:
- Title: ➤ Boundary-layer separation on isolated boattail nozzles
- Author: William Kelly Abeyounis
- Language: English
- Number of Pages: Median: 60
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Office - for sale by the National Technical Information Service
- Publish Date: 1978
- Publish Location: Washington - Springfield, Va
“Boundary-layer separation on isolated boattail nozzles” Subjects and Themes:
- Subjects: Jet nozzles - Airplanes - Laminar flow - Nacelles
Edition Identifiers:
- The Open Library ID: OL18014163M - OL17537910M - OL14932061M - OL15227214M - OL17979077M
Access and General Info:
- First Year Published: 1978
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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2Integration effects of D-shaped, underwing, aft-mounted, separate- flow, flow-through nacelles on a high-wing transport
By Milton Lamb
“Integration effects of D-shaped, underwing, aft-mounted, separate- flow, flow-through nacelles on a high-wing transport” Metadata:
- Title: ➤ Integration effects of D-shaped, underwing, aft-mounted, separate- flow, flow-through nacelles on a high-wing transport
- Author: Milton Lamb
- Language: English
- Number of Pages: Median: 21
- Publisher: ➤ Langley Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Division - For sale by the National Technical Information Service]
- Publish Date: 1987 - 1988
- Publish Location: ➤ [Washington, DC] - [Springfield, Va - Hampton, Va
“Integration effects of D-shaped, underwing, aft-mounted, separate- flow, flow-through nacelles on a high-wing transport” Subjects and Themes:
- Subjects: Airplanes - Nacelles - Wings - Aerodynamics - Wing nacelle configurations
Edition Identifiers:
- The Open Library ID: OL18030138M - OL19250458M - OL17096819M - OL15278150M
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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3XV-15 structural-acoustic data
By Karen H. Lyle
“XV-15 structural-acoustic data” Metadata:
- Title: XV-15 structural-acoustic data
- Author: Karen H. Lyle
- 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
“XV-15 structural-acoustic data” Subjects and Themes:
- Subjects: ➤ Tilting rotors - Horizontal flight - Flight conditions - Ground effect (Aerodynamics) - XV-15 aircraft - Hovering - Acoustic measurement - Noise intensity - Acoustic properties - Flight tests - Nacelles
Edition Identifiers:
- The Open Library ID: OL18131746M - OL17129388M - OL15538664M - OL17592996M
- Online Computer Library Center (OCLC) ID: 40989515
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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4An installed nacelle design code using a multiblock Euler solver
By H. C. Chen
“An installed nacelle design code using a multiblock Euler solver” Metadata:
- Title: ➤ An installed nacelle design code using a multiblock Euler solver
- Author: H. C. Chen
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1992
- Publish Location: ➤ Hampton, Va - [Springfield, Va.?
“An installed nacelle design code using a multiblock Euler solver” Subjects and Themes:
- Subjects: Nacelles - Airplanes - Design and construction
Edition Identifiers:
- The Open Library ID: OL15366353M - OL17786354M - OL17676514M - OL17786361M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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5Effect of underwing aft-mounted nacelles on the longitudinal aerodynamic characteristics of a high-wing transport airplane
By William Kelly Abeyounis
“Effect of underwing aft-mounted nacelles on the longitudinal aerodynamic characteristics of a high-wing transport airplane” Metadata:
- Title: ➤ Effect of underwing aft-mounted nacelles on the longitudinal aerodynamic characteristics of a high-wing transport airplane
- Author: William Kelly Abeyounis
- Language: English
- Number of Pages: Median: 136
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch - Langley Research Center
- Publish Date: 1985 - 1986
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.] - Hampton, Va
“Effect of underwing aft-mounted nacelles on the longitudinal aerodynamic characteristics of a high-wing transport airplane” Subjects and Themes:
- Subjects: Nacelles - Airplanes - Transport aircraft
Edition Identifiers:
- The Open Library ID: OL19985902M - OL18029594M - OL14664189M - OL15276241M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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6Installed nacelle drag-improvement tests of an M=0.8 turboprop transport configuration
By Alan D. Levin
“Installed nacelle drag-improvement tests of an M=0.8 turboprop transport configuration” Metadata:
- Title: ➤ Installed nacelle drag-improvement tests of an M=0.8 turboprop transport configuration
- Author: Alan D. Levin
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1983
- Publish Location: Moffett Field, Calif
“Installed nacelle drag-improvement tests of an M=0.8 turboprop transport configuration” Subjects and Themes:
- Subjects: Airplanes - Nacelles - Turbine-propeller engines
Edition Identifiers:
- The Open Library ID: OL17130407M - OL18042054M - OL17667525M - OL17082476M
Access and General Info:
- First Year Published: 1983
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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7B-1 AFT nacelle flow visualization study
By James L. Gunter
“B-1 AFT nacelle flow visualization study” Metadata:
- Title: ➤ B-1 AFT nacelle flow visualization study
- Author: James L. Gunter
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1975
- Publish Location: ➤ Springfield, Va - [Washington, DC
“B-1 AFT nacelle flow visualization study” Subjects and Themes:
- Subjects: ➤ B-1 aircraft - Cameras - Flight tests - Flow visualization - High speed photography - Nacelles
Edition Identifiers:
- The Open Library ID: OL18138796M - OL15561122M - OL17137446M - OL17592609M
- Online Computer Library Center (OCLC) ID: 43430687
Access and General Info:
- First Year Published: 1975
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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8Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle
By Milton Lamb
“Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle” Metadata:
- Title: ➤ Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle
- Author: Milton Lamb
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1985
- Publish Location: ➤ [Washington, D.C.] - Springfield, Va
“Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle” Subjects and Themes:
- Subjects: ➤ Statistics - Testing - Laminar flow - Turbulent flow - Pylons - Wing nacelle configurations - Wind tunnel tests - Airplanes - Transonic planes - Nacelles - Wings - Transport aircraft
Edition Identifiers:
- The Open Library ID: OL18217665M - OL18468463M - OL17724275M
- Online Computer Library Center (OCLC) ID: 776151030
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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9Design of 3-D nacelle near flat-plate wing using multiblock sensitivity analysis (ADOS)
By Mohamed E. Eleshaky
“Design of 3-D nacelle near flat-plate wing using multiblock sensitivity analysis (ADOS)” Metadata:
- Title: ➤ Design of 3-D nacelle near flat-plate wing using multiblock sensitivity analysis (ADOS)
- Author: Mohamed E. Eleshaky
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Design of 3-D nacelle near flat-plate wing using multiblock sensitivity analysis (ADOS)” Subjects and Themes:
- Subjects: Aircraft design - Design analysis - Drag reduction - Nacelles - Wing nacelle configuration
Edition Identifiers:
- The Open Library ID: OL15419482M - OL17078545M - OL18084619M
- Online Computer Library Center (OCLC) ID: 34608788
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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10Hover in-ground-effect testing of a full-scale, tilt-nacelle V/STOL model
By James E. Eshleman
“Hover in-ground-effect testing of a full-scale, tilt-nacelle V/STOL model” Metadata:
- Title: ➤ Hover in-ground-effect testing of a full-scale, tilt-nacelle V/STOL model
- Author: James E. Eshleman
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1986
- Publish Location: ➤ Moffett Field, Calif - [Springfield, Va
“Hover in-ground-effect testing of a full-scale, tilt-nacelle V/STOL model” Subjects and Themes:
- Subjects: Aerodynamics - Airplanes - Nacelles
Edition Identifiers:
- The Open Library ID: OL18030819M - OL17097489M - OL17659630M
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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11A grid-embedding transonic flow analysis computer program for wing/nacelle configurations
By Essam H. Atta
“A grid-embedding transonic flow analysis computer program for wing/nacelle configurations” Metadata:
- Title: ➤ A grid-embedding transonic flow analysis computer program for wing/nacelle configurations
- Author: Essam H. Atta
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1983
- Publish Location: Moffett Field, Calif
“A grid-embedding transonic flow analysis computer program for wing/nacelle configurations” Subjects and Themes:
- Subjects: Airplanes - Transonic planes - Nacelles
Edition Identifiers:
- The Open Library ID: OL18038220M - OL17555792M - OL15310341M
Access and General Info:
- First Year Published: 1983
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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12Theoretical flow characteristics of inlets for tilting-nacelle VTOL aircraft
By Michael A. Boles
“Theoretical flow characteristics of inlets for tilting-nacelle VTOL aircraft” Metadata:
- Title: ➤ Theoretical flow characteristics of inlets for tilting-nacelle VTOL aircraft
- Author: Michael A. Boles
- Language: English
- Number of Pages: Median: 29
- Publisher: ➤ for sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1978
- Publish Location: Springfield, Va - Washington
“Theoretical flow characteristics of inlets for tilting-nacelle VTOL aircraft” Subjects and Themes:
- Subjects: ➤ Airplanes - Vertically rising aircraft - Air intakes - Aerodynamics - Nacelles - Jet engines - Jet propulsion
Edition Identifiers:
- The Open Library ID: OL17647711M - OL17818398M
Access and General Info:
- First Year Published: 1978
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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13Installed nacelle drag-improvement tests of an M=0.8 turboprop transport configuration
By Alan D Levin
“Installed nacelle drag-improvement tests of an M=0.8 turboprop transport configuration” Metadata:
- Title: ➤ Installed nacelle drag-improvement tests of an M=0.8 turboprop transport configuration
- Author: Alan D Levin
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1983
- Publish Location: Moffett Field, Calif
“Installed nacelle drag-improvement tests of an M=0.8 turboprop transport configuration” Subjects and Themes:
- Subjects: Airplanes - Nacelles - Turbine-propeller engines
Edition Identifiers:
- The Open Library ID: OL17977344M - OL14926104M
Access and General Info:
- First Year Published: 1983
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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14Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration
By Lawrence E. Putnam
“Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration” Metadata:
- Title: ➤ Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration
- Author: Lawrence E. Putnam
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1986
- Publish Location: ➤ [Washington, D.C.] - Springfield, Va
“Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Airplanes - Body-wing configurations - Design and construction - Longitudinal Stability of airplanes - Nacelles - Stability of airplanes, Longitudinal - Transonic speed - Transport aircraft - Transport planes - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL16116642M - OL18218653M
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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15Short Haul Civil Tiltrotor study in MIDAS
By Adolph Atencio
“Short Haul Civil Tiltrotor study in MIDAS” Metadata:
- Title: ➤ Short Haul Civil Tiltrotor study in MIDAS
- Author: Adolph Atencio
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Short Haul Civil Tiltrotor study in MIDAS” Subjects and Themes:
- Subjects: ➤ Automatic control - Short haul aircraft - Manuals - Manual control - Man machine systems - Aircraft design - Nacelles
Edition Identifiers:
- The Open Library ID: OL17593149M - OL15542474M
- Online Computer Library Center (OCLC) ID: 42042470
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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16Installation effects of long-duct pylon-mounted nacelles on a twin-jet transport model with swept supercritical wing
By Edwin E. Lee
“Installation effects of long-duct pylon-mounted nacelles on a twin-jet transport model with swept supercritical wing” Metadata:
- Title: ➤ Installation effects of long-duct pylon-mounted nacelles on a twin-jet transport model with swept supercritical wing
- Author: Edwin E. Lee
- Language: English
- Number of Pages: Median: 142
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - Langley Research Center - For sale by the National Technical Information Service]
- Publish Date: 1985 - 1986
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, D.C.]
“Installation effects of long-duct pylon-mounted nacelles on a twin-jet transport model with swept supercritical wing” Subjects and Themes:
- Subjects: Nacelles - Airplanes - Supercritical wings - Twin-engine airplanes
Edition Identifiers:
- The Open Library ID: OL14664000M - OL19985947M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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17Effect of nacelles on aerodynamic characteristics of an executive-jet model with simulated, partial-chord, laminar-flow-control wing glove
By Richard L. Campbell
“Effect of nacelles on aerodynamic characteristics of an executive-jet model with simulated, partial-chord, laminar-flow-control wing glove” Metadata:
- Title: ➤ Effect of nacelles on aerodynamic characteristics of an executive-jet model with simulated, partial-chord, laminar-flow-control wing glove
- Author: Richard L. Campbell
- Language: English
- Number of Pages: Median: 101
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
- Publish Date: 1982
- Publish Location: ➤ [Springfield, Va - Washington, D.C
“Effect of nacelles on aerodynamic characteristics of an executive-jet model with simulated, partial-chord, laminar-flow-control wing glove” Subjects and Themes:
- Subjects: Aerodynamics, Transonic - Airplanes - Laminar flow - Nacelles - Transonic Aerodynamics
Edition Identifiers:
- The Open Library ID: OL17799262M - OL15260721M
Access and General Info:
- First Year Published: 1982
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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18Experimental and theoretical study of flow fields around ducted-nacelle models
By Robert J. Mack
“Experimental and theoretical study of flow fields around ducted-nacelle models” Metadata:
- Title: ➤ Experimental and theoretical study of flow fields around ducted-nacelle models
- Author: Robert J. Mack
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: Hampton, Va - [Springfield, Va
“Experimental and theoretical study of flow fields around ducted-nacelle models” Subjects and Themes:
- Subjects: ➤ Flow characteristics - Angle of attack - Ducted flow - Ducted bodies - Aircraft design - Fluid flow - Mach number - Nacelles
Edition Identifiers:
- The Open Library ID: OL17838725M - OL17700655M
- Online Computer Library Center (OCLC) ID: 41161421
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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19Effects of nacelle configuration/position on performance of subsonic transport
By L. H. Bangert
“Effects of nacelle configuration/position on performance of subsonic transport” Metadata:
- Title: ➤ Effects of nacelle configuration/position on performance of subsonic transport
- Author: L. H. Bangert
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1983
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“Effects of nacelle configuration/position on performance of subsonic transport” Subjects and Themes:
- Subjects: Aerodynamics - Airplanes - Nacelles
Edition Identifiers:
- The Open Library ID: OL17663273M - OL17830105M
Access and General Info:
- First Year Published: 1983
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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20Hover test results of a small-scale twin-tilt nacelle model
By Susan B. Schmidt
“Hover test results of a small-scale twin-tilt nacelle model” Metadata:
- Title: ➤ Hover test results of a small-scale twin-tilt nacelle model
- Author: Susan B. Schmidt
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1985
- Publish Location: Moffett Field, Calif
“Hover test results of a small-scale twin-tilt nacelle model” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL15273686M - OL17748299M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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21Finite difference time marching in the frequency domain
By Kenneth J. Baumeister
“Finite difference time marching in the frequency domain” Metadata:
- Title: ➤ Finite difference time marching in the frequency domain
- Author: Kenneth J. Baumeister
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, D.C - Springfield, Va - [Washington, DC
“Finite difference time marching in the frequency domain” Subjects and Themes:
- Subjects: ➤ Acoustics - Aircraft engines - Ducts - Engine inlets - Finite difference theory - Nacelles - Partial Differential equations - Sound propagation - Time dependence - Time marching - Wave equations
Edition Identifiers:
- The Open Library ID: OL15505882M - OL15503807M
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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22Interim note on tests with a wing-mounted fan nacelle with the fan jet simulated by cold air blowing and alternatively by a gas generator shroud
By G. Pauley
“Interim note on tests with a wing-mounted fan nacelle with the fan jet simulated by cold air blowing and alternatively by a gas generator shroud” Metadata:
- Title: ➤ Interim note on tests with a wing-mounted fan nacelle with the fan jet simulated by cold air blowing and alternatively by a gas generator shroud
- Author: G. Pauley
- Language: English
- Number of Pages: Median: 30
- Publisher: H.M. Stationery Off.
- Publish Date: 1970
- Publish Location: London
“Interim note on tests with a wing-mounted fan nacelle with the fan jet simulated by cold air blowing and alternatively by a gas generator shroud” Subjects and Themes:
- Subjects: Airplanes - Nacelles - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL4370877M
- Library of Congress Control Number (LCCN): 78555888
Access and General Info:
- First Year Published: 1970
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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23Wind tunnel tests on a streamlined fan-lift nacelle
By James Ernest Hackett
“Wind tunnel tests on a streamlined fan-lift nacelle” Metadata:
- Title: ➤ Wind tunnel tests on a streamlined fan-lift nacelle
- Author: James Ernest Hackett
- Language: English
- Number of Pages: Median: 50
- Publisher: H.M.S.O.
- Publish Date: 1967
- Publish Location: London
“Wind tunnel tests on a streamlined fan-lift nacelle” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL5588289M
- Online Computer Library Center (OCLC) ID: 6189279
- Library of Congress Control Number (LCCN): 67108694
Access and General Info:
- First Year Published: 1967
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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24Balance measurements (excluding drag) on a delta wing aircraft at transonic speeds
By M. M. Shaw
“Balance measurements (excluding drag) on a delta wing aircraft at transonic speeds” Metadata:
- Title: ➤ Balance measurements (excluding drag) on a delta wing aircraft at transonic speeds
- Author: M. M. Shaw
- Language: English
- Number of Pages: Median: 11
- Publisher: H.M.S.O.
- Publish Date: 1967
- Publish Location: London
“Balance measurements (excluding drag) on a delta wing aircraft at transonic speeds” Subjects and Themes:
- Subjects: ➤ Airplanes - Lateral Stability of airplanes - Lift (Aerodynamics) - Nacelles - Transonic Aerodynamics - Triangular Wings
Edition Identifiers:
- The Open Library ID: OL5574944M
- Library of Congress Control Number (LCCN): 67085771
Access and General Info:
- First Year Published: 1967
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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25Performance optimization of a rotor alone Nacelle for acoustic fan testing
By C. C. Cunningham
“Performance optimization of a rotor alone Nacelle for acoustic fan testing” Metadata:
- Title: ➤ Performance optimization of a rotor alone Nacelle for acoustic fan testing
- Author: C. C. Cunningham
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2000
- Publish Location: ➤ [Cleveland, Ohio] - Springfield, VA
“Performance optimization of a rotor alone Nacelle for acoustic fan testing” Subjects and Themes:
- Subjects: ➤ Acoustic properties - Automatic control - Error analysis - Nacelles - Rotor speed - Test chambers - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL16012049M
Access and General Info:
- First Year Published: 2000
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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26NASA acoustically treated nacelle program
By Langley Research Center
“NASA acoustically treated nacelle program” Metadata:
- Title: ➤ NASA acoustically treated nacelle program
- Author: Langley Research Center
- Language: English
- Number of Pages: Median: 165
- Publisher: ➤ Scientific and Technical Information Division, Office of Technology Utilization, National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.]
- Publish Date: 1969
- Publish Location: Washington
“NASA acoustically treated nacelle program” Subjects and Themes:
- Subjects: Airplanes - Noise - Congresses - Nacelles
Edition Identifiers:
- The Open Library ID: OL4854598M
- Library of Congress Control Number (LCCN): 75604634
Access and General Info:
- First Year Published: 1969
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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27SIMPROP
By Th. E. Labrujere
“SIMPROP” Metadata:
- Title: SIMPROP
- Author: Th. E. Labrujere
- Number of Pages: Median: 43
- Publisher: National Aerospace Laboratory
- Publish Date: 1984
- Publish Location: Amsterdam
“SIMPROP” Subjects and Themes:
- Subjects: ➤ Airfoils - Two dimensional flow - Transonic flow - Propellers - Spinners - Nacelles
Edition Identifiers:
- The Open Library ID: OL20982769M
Access and General Info:
- First Year Published: 1984
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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28Effects of varying podded nacelle-nozzle installations on transonic aeropropulsive characteristics of a supersonic fighter aircraft
By Francis J Capone
“Effects of varying podded nacelle-nozzle installations on transonic aeropropulsive characteristics of a supersonic fighter aircraft” Metadata:
- Title: ➤ Effects of varying podded nacelle-nozzle installations on transonic aeropropulsive characteristics of a supersonic fighter aircraft
- Author: Francis J Capone
- Language: English
- Number of Pages: Median: 334
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1983
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“Effects of varying podded nacelle-nozzle installations on transonic aeropropulsive characteristics of a supersonic fighter aircraft” Subjects and Themes:
- Subjects: ➤ Airplanes - Canard Wings - Nacelles - Supersonic planes - Transonic planes - Wings, Canard
Edition Identifiers:
- The Open Library ID: OL14933304M
Access and General Info:
- First Year Published: 1983
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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29Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport
By Milton Lamb
“Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport” Metadata:
- Title: ➤ Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport
- Author: Milton Lamb
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1986
- Publish Location: ➤ Washington, D.C - Springfield, Va
“Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport” Subjects and Themes:
- Subjects: ➤ Nacelles - Skin friction - Pylons - System effectiveness - Wind tunnel tests - Testing - Airplanes - Aerodynamic drag - Transonic planes - Wings
Edition Identifiers:
- The Open Library ID: OL16152786M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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30Some acoustic results from the Pratt and Whitney Advanced Ducted Propulsor
By James H. Dittmar
“Some acoustic results from the Pratt and Whitney Advanced Ducted Propulsor” Metadata:
- Title: ➤ Some acoustic results from the Pratt and Whitney Advanced Ducted Propulsor
- Author: James H. Dittmar
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 1999
- Publish Location: ➤ [Springfield, Va - [Cleveland, Ohio]
“Some acoustic results from the Pratt and Whitney Advanced Ducted Propulsor” Subjects and Themes:
- Subjects: ➤ Ducts - Engine design - Noise reduction - Effective perceived noise levels - Nacelles - Noise measurement
Edition Identifiers:
- The Open Library ID: OL17133231M
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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31Ducted fan acoustic radiation including the effects of nonuniform mean flow and acoustic treatment
By Walter Eversman
“Ducted fan acoustic radiation including the effects of nonuniform mean flow and acoustic treatment” Metadata:
- Title: ➤ Ducted fan acoustic radiation including the effects of nonuniform mean flow and acoustic treatment
- Author: Walter Eversman
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Dept. of Mechanical and Aerospace Engineering and Engineering Mechanics, Univ. of Missouri-Rolla
- Publish Date: 1993
- Publish Location: ➤ Springfield, Va - [Washington, DC - Rolla, Mo
“Ducted fan acoustic radiation including the effects of nonuniform mean flow and acoustic treatment” Subjects and Themes:
- Subjects: ➤ Fan blades - Acoustic propagation - Far fields - Ducted fan engines - Aerodynamic noise - Noise generators - Sound waves - Nonuniform flow - Nacelles
Edition Identifiers:
- The Open Library ID: OL15408456M
Access and General Info:
- First Year Published: 1993
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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32Fan 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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33On the solution of the three-dimensional flowfield about a flow-through nacelle
By William B. Compton
“On the solution of the three-dimensional flowfield about a flow-through nacelle” Metadata:
- Title: ➤ On the solution of the three-dimensional flowfield about a flow-through nacelle
- Author: William B. Compton
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration
- Publish Date: 1985
- Publish Location: [Washington DC
“On the solution of the three-dimensional flowfield about a flow-through nacelle” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL15296801M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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34Effects of nacelle configuration/position on performance of subsonic transport
By L. H Bangert
“Effects of nacelle configuration/position on performance of subsonic transport” Metadata:
- Title: ➤ Effects of nacelle configuration/position on performance of subsonic transport
- Author: L. H Bangert
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
- Publish Date: 1983
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“Effects of nacelle configuration/position on performance of subsonic transport” Subjects and Themes:
- Subjects: Aerodynamics - Airplanes - Nacelles
Edition Identifiers:
- The Open Library ID: OL14931260M
Access and General Info:
- First Year Published: 1983
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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35Theoretical study of VTOL tilt-nacelle axisymmetric inlet geometries
By J. Dennis Hawk
“Theoretical study of VTOL tilt-nacelle axisymmetric inlet geometries” Metadata:
- Title: ➤ Theoretical study of VTOL tilt-nacelle axisymmetric inlet geometries
- Author: J. Dennis Hawk
- Language: English
- Number of Pages: Median: 26
- Publisher: ➤ for sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1979
- Publish Location: Springfield, Va - [Washington]
“Theoretical study of VTOL tilt-nacelle axisymmetric inlet geometries” Subjects and Themes:
- Subjects: Airplanes - Air intakes - Vertically rising aircraft - Nacelles - Turbojet engines
Edition Identifiers:
- The Open Library ID: OL15229388M
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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36Theoretical flow characteristics of inlets for tilting-nacelle VTOL aircraft
By Michael A Boles
“Theoretical flow characteristics of inlets for tilting-nacelle VTOL aircraft” Metadata:
- Title: ➤ Theoretical flow characteristics of inlets for tilting-nacelle VTOL aircraft
- Author: Michael A Boles
- Language: English
- Number of Pages: Median: 29
- Publisher: ➤ for sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1978
- Publish Location: Springfield, Va - Washington
“Theoretical flow characteristics of inlets for tilting-nacelle VTOL aircraft” Subjects and Themes:
- Subjects: ➤ Vertically rising aircraft - Air intakes - Aerodynamics - Jet engines - Airplanes - Nacelles
Edition Identifiers:
- The Open Library ID: OL14932027M
Access and General Info:
- First Year Published: 1978
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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37Installation effects of wing-mounted turbofan nacelle-pylons on a 1/17-scale, twin-engine, low-wing transport model
By Odis C. Pendergraft
“Installation effects of wing-mounted turbofan nacelle-pylons on a 1/17-scale, twin-engine, low-wing transport model” Metadata:
- Title: ➤ Installation effects of wing-mounted turbofan nacelle-pylons on a 1/17-scale, twin-engine, low-wing transport model
- Author: Odis C. Pendergraft
- Number of Pages: Median: 105
- Publisher: Langley Research Center
- Publish Date: 1992
- Publish Location: Hampton, Va
“Installation effects of wing-mounted turbofan nacelle-pylons on a 1/17-scale, twin-engine, low-wing transport model” Subjects and Themes:
- Subjects: Low wing aircraft - Nacelles
Edition Identifiers:
- The Open Library ID: OL21379276M
Author's Alternative Names:
"Odis C Pendergraft"Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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38Aircraft drag prediction and reduction: computational drag analyses and minimization; mission impossible?
By J. W. Slooff
“Aircraft drag prediction and reduction: computational drag analyses and minimization; mission impossible?” Metadata:
- Title: ➤ Aircraft drag prediction and reduction: computational drag analyses and minimization; mission impossible?
- Author: J. W. Slooff
- Number of Pages: Median: 24
- Publisher: AGARD
- Publish Date: 1986
- Publish Location: Neuilly sur Seine, France
“Aircraft drag prediction and reduction: computational drag analyses and minimization; mission impossible?” Subjects and Themes:
- Subjects: ➤ Skin friction - Boundary layers - Aerodynamic drag - Turbulence - External stores - Laminar flow - Nacelles
Edition Identifiers:
- The Open Library ID: OL19987104M
Author's Alternative Names:
"Johannes W. Slooff", "Joop Slooff" and "J.W. Slooff"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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39Effect of location of aft-mounted nacelles on longitudinal aerodynamic characteristics of a high-wing transport
By William Kelly Abeyounis
“Effect of location of aft-mounted nacelles on longitudinal aerodynamic characteristics of a high-wing transport” Metadata:
- Title: ➤ Effect of location of aft-mounted nacelles on longitudinal aerodynamic characteristics of a high-wing transport
- Author: William Kelly Abeyounis
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service]
- Publish Date: 1990
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Effect of location of aft-mounted nacelles on longitudinal aerodynamic characteristics of a high-wing transport” Subjects and Themes:
- Subjects: Airplanes - Transport planes - Nacelles
Edition Identifiers:
- The Open Library ID: OL15368328M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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40Effect of location of aft-mounted nacelles on longitudinal aerodynamic characteristics of a high-wing transport airplane
By William Kelly Abeyounis
“Effect of location of aft-mounted nacelles on longitudinal aerodynamic characteristics of a high-wing transport airplane” Metadata:
- Title: ➤ Effect of location of aft-mounted nacelles on longitudinal aerodynamic characteristics of a high-wing transport airplane
- Author: William Kelly Abeyounis
- Number of Pages: Median: 95
- Publisher: Langley Research Center
- Publish Date: 1990
- Publish Location: Hampton, Va
“Effect of location of aft-mounted nacelles on longitudinal aerodynamic characteristics of a high-wing transport airplane” Subjects and Themes:
- Subjects: Aerodynamic characteristics - Transport aircraft - Nacelles
Edition Identifiers:
- The Open Library ID: OL21334723M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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41Advanced turbofan duct liner concepts
By Gerald W. Bielak
“Advanced turbofan duct liner concepts” Metadata:
- Title: ➤ Advanced turbofan duct liner concepts
- Author: Gerald W. Bielak
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1999
- Publish Location: Hampton, Va - [Springfield, Va
“Advanced turbofan duct liner concepts” Subjects and Themes:
- Subjects: ➤ Aircraft noise - Acoustic attenuation - Turbofan engines - Linings - Acoustic ducts - Noise reduction - Nacelles
Edition Identifiers:
- The Open Library ID: OL15548395M
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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42Supersonic flow visualization of a nacelle in close proximity to a simulated wing
By Kasim Biber
“Supersonic flow visualization of a nacelle in close proximity to a simulated wing” Metadata:
- Title: ➤ Supersonic flow visualization of a nacelle in close proximity to a simulated wing
- Author: Kasim Biber
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Institute for Aviation Research, Wichita State University - National Technical Information Service, distributor
- Publish Date: 1993
- Publish Location: ➤ [Washington, DC - Springfield, Va - Wichita, Kan
“Supersonic flow visualization of a nacelle in close proximity to a simulated wing” Subjects and Themes:
- Subjects: Wind tunnels - Airplanes - Flow visualization - Nacelles
Edition Identifiers:
- The Open Library ID: OL14699718M
Access and General Info:
- First Year Published: 1993
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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43Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds
By Robert J. Mack
“Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds” Metadata:
- Title: ➤ Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds
- Author: Robert J. Mack
- 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
“Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds” Subjects and Themes:
- Subjects: ➤ Body-wing configurations - Wind tunnel tests - Aerodynamic characteristics - Supersonic flight - Aerodynamic noise - Noise reduction - Sonic booms - Aerodynamic configurations - Wings - Nacelles
Edition Identifiers:
- The Open Library ID: OL15566524M
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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44Experimental determination of flow-interference effects of wing-mounted two-dimensional, full-capture propulsion nacelles in close proximity to a vehicle body at a Mach number of 6
By Walter A Vahl
“Experimental determination of flow-interference effects of wing-mounted two-dimensional, full-capture propulsion nacelles in close proximity to a vehicle body at a Mach number of 6” Metadata:
- Title: ➤ Experimental determination of flow-interference effects of wing-mounted two-dimensional, full-capture propulsion nacelles in close proximity to a vehicle body at a Mach number of 6
- Author: Walter A Vahl
- Language: English
- Number of Pages: Median: 33
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1982
- Publish Location: ➤ [Springfield, Va - Washington, D.C
“Experimental determination of flow-interference effects of wing-mounted two-dimensional, full-capture propulsion nacelles in close proximity to a vehicle body at a Mach number of 6” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Aerodynamics, Hypersonic - Airplanes - Hypersonic Aerodynamics - Nacelles - Testing
Edition Identifiers:
- The Open Library ID: OL16806739M
Access and General Info:
- First Year Published: 1982
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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45Drag measurements of an axisymmetric nacelle mounted on a flat plate at supersonic speeds
By Jeffrey D. Flamm
“Drag measurements of an axisymmetric nacelle mounted on a flat plate at supersonic speeds” Metadata:
- Title: ➤ Drag measurements of an axisymmetric nacelle mounted on a flat plate at supersonic speeds
- Author: Jeffrey D. Flamm
- Language: English
- Number of Pages: Median: 32
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - Available from the National Technical Information Service
- Publish Date: 1995
- Publish Location: ➤ [Hampton, Va.] - Springfield, VA
“Drag measurements of an axisymmetric nacelle mounted on a flat plate at supersonic speeds” Subjects and Themes:
- Subjects: Aerodynamics, Supersonic - Airplanes - Drag (Aerodynamics) - Nacelles - Supersonic Aerodynamics
Edition Identifiers:
- The Open Library ID: OL17141243M
- Online Computer Library Center (OCLC) ID: 32818274
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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46A computer program for the calculation of three-dimensional transonic nacelle/inlet flowfields
By Joseph Vadyak
“A computer program for the calculation of three-dimensional transonic nacelle/inlet flowfields” Metadata:
- Title: ➤ A computer program for the calculation of three-dimensional transonic nacelle/inlet flowfields
- Author: Joseph Vadyak
- Language: English
- Publisher: The Center
- Publish Date: 1983
- Publish Location: Moffett Field, Calif
“A computer program for the calculation of three-dimensional transonic nacelle/inlet flowfields” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL15310339M
Access and General Info:
- First Year Published: 1983
- 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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47Study to improve airframe turbine engine rotor blade containment
By C. O. Gunderson
“Study to improve airframe turbine engine rotor blade containment” Metadata:
- Title: ➤ Study to improve airframe turbine engine rotor blade containment
- Author: C. O. Gunderson
- Language: English
- Number of Pages: Median: 212
- Publisher: ➤ Dept. of Transportation, Federal Aviation Administration, Systems Research and Development Service - for sale by the National Technical Information Service
- Publish Date: 1977
- Publish Location: Washington - Springfield, Va
“Study to improve airframe turbine engine rotor blade containment” Subjects and Themes:
- Subjects: Design and construction - Airframes - Airplanes - Nacelles
Edition Identifiers:
- The Open Library ID: OL15217781M
Access and General Info:
- First Year Published: 1977
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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48Analysis of results from wind tunnel tests of inlets for an advanced turboprop nacelle installation
By J. P. Hancock
“Analysis of results from wind tunnel tests of inlets for an advanced turboprop nacelle installation” Metadata:
- Title: ➤ Analysis of results from wind tunnel tests of inlets for an advanced turboprop nacelle installation
- Author: J. P. Hancock
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration
- Publish Date: 1989
- Publish Location: [Washington, DC]
“Analysis of results from wind tunnel tests of inlets for an advanced turboprop nacelle installation” Subjects and Themes:
- Subjects: Airplanes - Turbine-propeller engines - Testing - Nacelles
Edition Identifiers:
- The Open Library ID: OL15281803M
Access and General Info:
- First Year Published: 1989
- 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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49Interactive calculation procedures for mixed compression inlets
By Eli Reshotko
“Interactive calculation procedures for mixed compression inlets” Metadata:
- Title: ➤ Interactive calculation procedures for mixed compression inlets
- Author: Eli Reshotko
- Language: English
- Publisher: ➤ Dept. of Mechanical and Aerospace Engineering, School of Engineering, Case Institute of Technology, Case Western Reserve University
- Publish Date: 1983
- Publish Location: Cleveland, Ohio
“Interactive calculation procedures for mixed compression inlets” Subjects and Themes:
- Subjects: ➤ Supersonic aircraft - Laminar boundary layer - Turbulent boundary layer - Shock wave interaction - Oblique shock waves - Nacelles
Edition Identifiers:
- The Open Library ID: OL16125496M
Access and General Info:
- First Year Published: 1983
- 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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50An analysis of the Wright Patterson full-scale engine nacelle fire suppression experiments
By Anthony Hamins
“An analysis of the Wright Patterson full-scale engine nacelle fire suppression experiments” Metadata:
- Title: ➤ An analysis of the Wright Patterson full-scale engine nacelle fire suppression experiments
- Author: Anthony Hamins
- Language: English
- Number of Pages: Median: 84
- Publisher: ➤ U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology
- Publish Date: 1997
- Publish Location: Gaithersburg, MD
“An analysis of the Wright Patterson full-scale engine nacelle fire suppression experiments” Subjects and Themes:
- Subjects: ➤ Fires and fire prevention - Fire extinction - Testing - Airplanes - Chemical systems - Nacelles
Edition Identifiers:
- The Open Library ID: OL13567588M
- Online Computer Library Center (OCLC) ID: 40747164
Access and General Info:
- First Year Published: 1997
- 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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