Explore: Turbocompressors
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AI-Generated Overview About “turbocompressors”:
Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1NASA low-speed axial compressor for fundamental research
By Charles A. Wasserbauer
“NASA low-speed axial compressor for fundamental research” Metadata:
- Title: ➤ NASA low-speed axial compressor for fundamental research
- Author: Charles A. Wasserbauer
- Language: English
- Number of Pages: Median: 11
- Publisher: ➤ Lewis Research Center - National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1995
- Publish Location: ➤ Cleveland, Ohio - [Washington, D.C.] - [Springfield, Va - [Washington, DC]
“NASA low-speed axial compressor for fundamental research” Subjects and Themes:
- Subjects: ➤ Turbocompressors - Test facilities - Hubs - Cases (Containers) - Internal flow - Low speed - Compressor blades
Edition Identifiers:
- The Open Library ID: ➤ OL19001848M - OL15417892M - OL18079904M - OL17012100M - OL18083441M - OL15411404M - OL17115000M - OL16984621M
- Online Computer Library Center (OCLC) ID: 33957706 - 32889675
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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2Off-design computer code for calculating the aerodynamic performance of axial-flow fans and compressors
By James F. Schmidt
“Off-design computer code for calculating the aerodynamic performance of axial-flow fans and compressors” Metadata:
- Title: ➤ Off-design computer code for calculating the aerodynamic performance of axial-flow fans and compressors
- Author: James F. Schmidt
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Off-design computer code for calculating the aerodynamic performance of axial-flow fans and compressors” Subjects and Themes:
- Subjects: ➤ Applications programs (Computers) - Axial flow - Axisymmetric flow - Performance prediction - Rotor aerodynamics - Steady flow - Turbocompressors - Turbofans - User manuals (Computer programs)
Edition Identifiers:
- The Open Library ID: OL17107865M - OL18086876M - OL15423145M
- Online Computer Library Center (OCLC) ID: 35248220
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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3Design of 9.271-pressure-ratio five-stage core compressor and overall performance for first three stages
By Ronald J. Steinke
“Design of 9.271-pressure-ratio five-stage core compressor and overall performance for first three stages” Metadata:
- Title: ➤ Design of 9.271-pressure-ratio five-stage core compressor and overall performance for first three stages
- Author: Ronald J. Steinke
- Language: English
- Number of Pages: Median: 32
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - Lewis Research Center - For sale by the National Technical Information Service]
- Publish Date: 1986 - 1987
- Publish Location: ➤ Cleveland, Ohio - [Springfield, Va - [Washington, D.C.]
“Design of 9.271-pressure-ratio five-stage core compressor and overall performance for first three stages” Subjects and Themes:
- Subjects: Compressors - Axial flow compressors - Turbocompressors
Edition Identifiers:
- The Open Library ID: OL15274135M - OL20899252M - OL18028604M - OL14663122M
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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4Enhanced capabilities and modified users manual for axial-flow compressor conceptual design code CSPAN
By Arthur J. Glassman
“Enhanced capabilities and modified users manual for axial-flow compressor conceptual design code CSPAN” Metadata:
- Title: ➤ Enhanced capabilities and modified users manual for axial-flow compressor conceptual design code CSPAN
- Author: Arthur J. Glassman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Enhanced capabilities and modified users manual for axial-flow compressor conceptual design code CSPAN” Subjects and Themes:
- Subjects: ➤ Applications programs (Computers) - Cascade flow - Computer aided design - Turbocompressors - User manuals (Computer programs)
Edition Identifiers:
- The Open Library ID: OL17790930M - OL15410016M
- Online Computer Library Center (OCLC) ID: 32823217
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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5WINCLR
By Bose, T. K.
“WINCLR” Metadata:
- Title: WINCLR
- Author: Bose, T. K.
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“WINCLR” Subjects and Themes:
- Subjects: ➤ Aircraft safety - Applications programs (Computers) - Clearances - Heat transfer - Ingestion (Engines) - Turbocompressors - User manuals (Computer programs) - Weather
Edition Identifiers:
- The Open Library ID: OL17017583M - OL17683978M
- Online Computer Library Center (OCLC) ID: 33425805
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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6Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor
By Kenneth L. Suder
“Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor” Metadata:
- Title: ➤ Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor
- Author: Kenneth L. Suder
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor” Subjects and Themes:
- Subjects: ➤ Air speed - Airspeed - Applications programs (Computers) - Blade tips - Blade-vortex interaction - Compressor rotors - Laser anemometers - Shock wave interaction - Tip speed - Transonic compressors - Turbo compressors - Turbocompressors - Vortices - Wall flow
Edition Identifiers:
- The Open Library ID: OL17791893M - OL15414396M
- Online Computer Library Center (OCLC) ID: 34041388
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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7Demonstration of PIV in a transonic compressor
By Mark P. Wernet
“Demonstration of PIV in a transonic compressor” Metadata:
- Title: ➤ Demonstration of PIV in a transonic compressor
- Author: Mark P. Wernet
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - [Cleveland, Ohio]
“Demonstration of PIV in a transonic compressor” Subjects and Themes:
- Subjects: Transonic compressors - Particle image velocimetry - Turbocompressors
Edition Identifiers:
- The Open Library ID: OL15539878M - OL17838311M
- Online Computer Library Center (OCLC) ID: 40758761
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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8Blading design for axial turbomachines
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
“Blading design for axial turbomachines” Metadata:
- Title: ➤ Blading design for axial turbomachines
- Author: ➤ North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
- Publisher: AGARD
- Publish Date: 1989
- Publish Location: Neuilly sur Seine, France
“Blading design for axial turbomachines” Subjects and Themes:
- Subjects: Aircraft engines - Axial flow turbines - Turbocompressors
Edition Identifiers:
- The Open Library ID: OL19379587M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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9Forced response testing of an axi-centrifugal turboshaft engine
By A. Karl Owen
“Forced response testing of an axi-centrifugal turboshaft engine” Metadata:
- Title: ➤ Forced response testing of an axi-centrifugal turboshaft engine
- Author: A. Karl Owen
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, U.S. Army Research Laboratory - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Forced response testing of an axi-centrifugal turboshaft engine” Subjects and Themes:
- Subjects: ➤ Dynamic response - Frequency distribution - Traveling waves - Energy transfer - Turbocompressors - Gas turbine engines - Rotating stalls - Turboshafts - Fourier analysis
Edition Identifiers:
- The Open Library ID: OL17807037M
- Online Computer Library Center (OCLC) ID: 38146530
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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10Effects of stator indexing on performance in a low speed multistage axial compressor
By Wendy S. Barankiewicz
“Effects of stator indexing on performance in a low speed multistage axial compressor” Metadata:
- Title: ➤ Effects of stator indexing on performance in a low speed multistage axial compressor
- Author: Wendy S. Barankiewicz
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Effects of stator indexing on performance in a low speed multistage axial compressor” Subjects and Themes:
- Subjects: Low speed - Stators - Losses - Turbocompressors - Stator blades
Edition Identifiers:
- The Open Library ID: OL15498502M
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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11Design geometry and design/off-design performance computer codes for compressors and turbines
By Arthur J. Glassman
“Design geometry and design/off-design performance computer codes for compressors and turbines” Metadata:
- Title: ➤ Design geometry and design/off-design performance computer codes for compressors and turbines
- Author: Arthur J. Glassman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Design geometry and design/off-design performance computer codes for compressors and turbines” Subjects and Themes:
- Subjects: ➤ Computational geometry - Engine design - Propulsion system performance - Turbocompressors - Propulsion system configurations - Gas turbine engines - Performance prediction - Applications programs (Computers) - Computer aided design
Edition Identifiers:
- The Open Library ID: OL15423409M
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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12Small engine technology
By Jeff L. Hansen
“Small engine technology” Metadata:
- Title: Small engine technology
- Author: Jeff L. Hansen
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Small engine technology” Subjects and Themes:
- Subjects: Turboshafts - Turbomachinery - Engine design - Turbocompressors - Pressure ratio
Edition Identifiers:
- The Open Library ID: OL17130989M
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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13User's guide for MSAP2D
By T. S. R. Reddy
“User's guide for MSAP2D” Metadata:
- Title: User's guide for MSAP2D
- Author: T. S. R. Reddy
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - [Washington, DC
“User's guide for MSAP2D” Subjects and Themes:
- Subjects: ➤ Dynamic response - Unsteady aerodynamics - User manuals (Computer programs) - Rotor blades (Turbomachinery) - Turbocompressors - Computer programs - Aeroelasticity - Flutter
Edition Identifiers:
- The Open Library ID: OL15505221M
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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14Investigation of axial positioning for flexural compressors
By Peter Riggle
“Investigation of axial positioning for flexural compressors” Metadata:
- Title: ➤ Investigation of axial positioning for flexural compressors
- Author: Peter Riggle
- Language: English
- Publisher: ➤ Goddard Space Flight Center - Tri-Cities University Center, University of Washington
- Publish Date: 1991
- Publish Location: ➤ [Greenbelt, Md.] - Richland, WA
“Investigation of axial positioning for flexural compressors” Subjects and Themes:
- Subjects: ➤ Compressors - Positioning - Static tests - Turbocompressors - Experiment design - Dynamic tests - Axial flow compressors - Magnetic measurement
Edition Identifiers:
- The Open Library ID: OL16132978M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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15A final report on NASA grant NGL-22-009-383 entitled Unsteady design-point flow phenomena in transonic compressors
By J. R. Gertz
“A final report on NASA grant NGL-22-009-383 entitled Unsteady design-point flow phenomena in transonic compressors” Metadata:
- Title: ➤ A final report on NASA grant NGL-22-009-383 entitled Unsteady design-point flow phenomena in transonic compressors
- Author: J. R. Gertz
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Gas Turbine Laboratory, Dept. of Aeronautics and Astronautics, Massachusetts Institute of Technology - National Aeronautics and Space Administration
- Publish Date: 1986
- Publish Location: ➤ Springfield, Va - [Washington, DC - Cambridge, MA
“A final report on NASA grant NGL-22-009-383 entitled Unsteady design-point flow phenomena in transonic compressors” Subjects and Themes:
- Subjects: ➤ Unsteady flow - Wakes - Transonic compressors - Compressor rotors - Turbocompressors - Flow distribution
Edition Identifiers:
- The Open Library ID: OL17684340M
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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16Aerodynamic broadband noise mechanisms applicable to axial compressors
By Robert A. Arnoldi
“Aerodynamic broadband noise mechanisms applicable to axial compressors” Metadata:
- Title: ➤ Aerodynamic broadband noise mechanisms applicable to axial compressors
- Author: Robert A. Arnoldi
- Number of Pages: Median: 38
- Publisher: ➤ Pratt & Whitney Aircraft Division of United Aircraft Corporation
- Publish Date: 1970
- Publish Location: [S.l.]
“Aerodynamic broadband noise mechanisms applicable to axial compressors” Subjects and Themes:
- Subjects: Broadband noise - Turbocompressors
Edition Identifiers:
- The Open Library ID: OL21333613M
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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17Final technical report on grant NAG3-1567 entitled Inlet distortion in engines on VSTOL aircraft
By Choon Sooi Tan
“Final technical report on grant NAG3-1567 entitled Inlet distortion in engines on VSTOL aircraft” Metadata:
- Title: ➤ Final technical report on grant NAG3-1567 entitled Inlet distortion in engines on VSTOL aircraft
- Author: Choon Sooi Tan
- Language: English
- Publisher: ➤ The Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ Cleveland, OH - [Springfield, Va
“Final technical report on grant NAG3-1567 entitled Inlet distortion in engines on VSTOL aircraft” Subjects and Themes:
- Subjects: ➤ Engine inlets - Flow distortion - Nonuniform flow - V/STOL aircraft - Three dimensional flow - Inlet flow - Turbocompressors
Edition Identifiers:
- The Open Library ID: OL18075768M
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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18Aeropropulsion technology (APT)
By N. J. Heidegger
“Aeropropulsion technology (APT)” Metadata:
- Title: ➤ Aeropropulsion technology (APT)
- Author: N. J. Heidegger
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Aeropropulsion technology (APT)” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Turbocompressors - Navier-Stokes equation - Aircraft engines - Grid generation (Mathematics) - Cavity flow - Stator blades - Labyrinth seals - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15505195M
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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19PIV for turbomachinery applications
By Mark P. Wernet
“PIV for turbomachinery applications” Metadata:
- Title: ➤ PIV for turbomachinery applications
- Author: Mark P. Wernet
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“PIV for turbomachinery applications” Subjects and Themes:
- Subjects: ➤ Equilibrium flow - Laser Doppler velocimeters - Particle image velocimetry - Transonic compressors - Turbocompressors - Turbomachinery - Unsteady flow - Velocity measurement
Edition Identifiers:
- The Open Library ID: OL15498060M
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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20Effects of shrouded stator cavity flows on multistage axial compressor aerodynamic performance
By Steven R. Wellborn
“Effects of shrouded stator cavity flows on multistage axial compressor aerodynamic performance” Metadata:
- Title: ➤ Effects of shrouded stator cavity flows on multistage axial compressor aerodynamic performance
- Author: Steven R. Wellborn
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Effects of shrouded stator cavity flows on multistage axial compressor aerodynamic performance” Subjects and Themes:
- Subjects: ➤ Losses - Turbocompressors - Aerodynamic characteristics - Degradation - Turbomachinery - Stator blades - Rotors - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15491905M
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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21Axial-flow compressor noise (generation, transmission and radiation of discrete frequency components)
By Shojiro Kaji
“Axial-flow compressor noise (generation, transmission and radiation of discrete frequency components)” Metadata:
- Title: ➤ Axial-flow compressor noise (generation, transmission and radiation of discrete frequency components)
- Author: Shojiro Kaji
- Publisher: Sine nomine
- Publish Location: [Japan?]
“Axial-flow compressor noise (generation, transmission and radiation of discrete frequency components)” Subjects and Themes:
- Subjects: Noise - Turbocompressors
Edition Identifiers:
- The Open Library ID: OL20268518M
Access and General Info:
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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22Inlet flow test calibration for a small axial compressor facility
By D. P. Miller
“Inlet flow test calibration for a small axial compressor facility” Metadata:
- Title: ➤ Inlet flow test calibration for a small axial compressor facility
- Author: D. P. Miller
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1994
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Inlet flow test calibration for a small axial compressor facility” Subjects and Themes:
- Subjects: Test facilities - Calibrating - Inlet flow - Turbocompressors - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15404302M
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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23Inlet flow test calibration for a small axial compressor rig
By D. P. Miller
“Inlet flow test calibration for a small axial compressor rig” Metadata:
- Title: ➤ Inlet flow test calibration for a small axial compressor rig
- Author: D. P. Miller
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Inlet flow test calibration for a small axial compressor rig” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Axisymmetric flow - Test stands - Calibrating - Engine testing laboratories - Inlet flow - Turbocompressors
Edition Identifiers:
- The Open Library ID: OL15414468M
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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24Dimension determination of precursive stall events in a single stage high speed compressor
By Michelle M. Bright
“Dimension determination of precursive stall events in a single stage high speed compressor” Metadata:
- Title: ➤ Dimension determination of precursive stall events in a single stage high speed compressor
- Author: Michelle M. Bright
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Dimension determination of precursive stall events in a single stage high speed compressor” Subjects and Themes:
- Subjects: Pressure measurement - Power spectra - Turbocompressors - Rotating stalls - Chaos
Edition Identifiers:
- The Open Library ID: OL15496505M
Access and General Info:
- First Year Published: 1996
- 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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25Static flow characteristics of a mass flow injecting valve
By Duane L. Mattern
“Static flow characteristics of a mass flow injecting valve” Metadata:
- Title: ➤ Static flow characteristics of a mass flow injecting valve
- Author: Duane L. Mattern
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Static flow characteristics of a mass flow injecting valve” Subjects and Themes:
- Subjects: ➤ Static characteristics - Orifice flow - Steady flow - Flow characteristics - Valves - Turbocompressors - Design analysis
Edition Identifiers:
- The Open Library ID: OL15424033M
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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26Unsteady flows in a single-stage transonic axial-flow fan stator row
By Michael D. Hathaway
“Unsteady flows in a single-stage transonic axial-flow fan stator row” Metadata:
- Title: ➤ Unsteady flows in a single-stage transonic axial-flow fan stator row
- Author: Michael D. Hathaway
- Language: English
- Number of Pages: Median: 200
- Publisher: ➤ U.S. Army Aviation Systems Command - National Aeronautics and Space Administration - For sale by the National Technical Information Service
- Publish Date: 1986
- Publish Location: ➤ [Springfield, Va - [St. Louis, MO] - [Washington, D.C.]
“Unsteady flows in a single-stage transonic axial-flow fan stator row” Subjects and Themes:
- Subjects: ➤ Axial flow turbines - Measurement - Performance - Stator blades - Transonic flow - Turbo engines - Turbocompressors - Turboengines - Turbomachines - Unsteady flow - Unsteady flow (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL15415423M
Access and General Info:
- First Year Published: 1986
- 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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27Secondary flow spanwise deviation model for the stators of NASA middle compressor stages
By William B. Roberts
“Secondary flow spanwise deviation model for the stators of NASA middle compressor stages” Metadata:
- Title: ➤ Secondary flow spanwise deviation model for the stators of NASA middle compressor stages
- Author: William B. Roberts
- Language: English
- Publisher: Lewis Research Center
- Publish Date: 1984
- Publish Location: Cleveland, Ohio
“Secondary flow spanwise deviation model for the stators of NASA middle compressor stages” Subjects and Themes:
- Subjects: ➤ Compressors - Deviation - Airplanes - Turbocompressors - Mathematical models - Secondary flow - Stators - Compressor blades - Blades
Edition Identifiers:
- The Open Library ID: OL16153867M
Access and General Info:
- First Year Published: 1984
- 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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28Application of modified loss and deviation correlations to transonic axial compressors
By M. Cetin
“Application of modified loss and deviation correlations to transonic axial compressors” Metadata:
- Title: ➤ Application of modified loss and deviation correlations to transonic axial compressors
- Author: M. Cetin
- Number of Pages: Median: 64
- Publisher: AGARD
- Publish Date: 1987
- Publish Location: Neuilly sur Seine, France
“Application of modified loss and deviation correlations to transonic axial compressors” Subjects and Themes:
- Subjects: Transonic flow - Turbocompressors
Edition Identifiers:
- The Open Library ID: OL20897920M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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29Rotordynamics and design methods of an oil-free turbocharger
By Samuel A. Howard
“Rotordynamics and design methods of an oil-free turbocharger” Metadata:
- Title: ➤ Rotordynamics and design methods of an oil-free turbocharger
- Author: Samuel A. Howard
- Language: English
- Publisher: ➤ National Technical Information Service [distributor - National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1999
- Publish Location: ➤ Springfield, VA - [Cleveland, Ohio]
“Rotordynamics and design methods of an oil-free turbocharger” Subjects and Themes:
- Subjects: ➤ Design analysis - Foil bearings - Gas bearings - Rotor dynamics - Superchargers - Turbocompressors
Edition Identifiers:
- The Open Library ID: OL15542609M
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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Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
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tools for plant and network operators Air pollution control equipment Turbocompressors for petrochemical, refining, oil and gas, and chemical applications
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power) slightly higher speeds and were non-reversible. To accommodate turbocompressors and other additional systems, exhaust manifolds were enlarged and various
Cameron International
Group, founded in 1955 in Buffalo, New York, which was renamed Cooper Turbocompressor as part of Cooper Compression. W-K-M valves company, established in
Howden Turbo
acquisition of Howden. "KK&K: A full range of world class industrial turbocompressors and steam turbines". "Siemens Frankenthal jetzt in schottischen Händen"
Auguste Rateau
This entity manages the maintenance of turbomachines, turbo-pumps and turbocompressors installed on nuclear, thermal and industrial sites in France and in