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Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Turbine blade-tip clearance excitation forces
By Manuel Martinez-Sanchez
“Turbine blade-tip clearance excitation forces” Metadata:
- Title: ➤ Turbine blade-tip clearance excitation forces
- Author: Manuel Martinez-Sanchez
- Language: English
- Number of Pages: Median: 91
- Publisher: ➤ National Technical Information Service, distributor - Massachusetts Institute of Technology - National Aeronautics and Space Administration
- Publish Date: 1985
- Publish Location: ➤ Cambridge, Mass - Springfield, Va - [Washington, DC
“Turbine blade-tip clearance excitation forces” Subjects and Themes:
- Subjects: ➤ Aerodynamic forces - Blade tips - Blades - Flow distribution - Force distribution - Self excitation - Turbine blades - Turbines - Turbomachines - Vibration
Edition Identifiers:
- The Open Library ID: OL18082277M - OL14984718M - OL15415419M - OL18007699M
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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2Passage-averaged description of wave rotor flow
By Gerard E. Welch
“Passage-averaged description of wave rotor flow” Metadata:
- Title: ➤ Passage-averaged description of wave rotor flow
- Author: Gerard E. Welch
- Language: English
- Publisher: ➤ U.S. Army Research Laboratory, Lewis Research Center - Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1997
- Publish Location: ➤ [Cleveland, Ohio] - [Hanover, MD
“Passage-averaged description of wave rotor flow” Subjects and Themes:
- Subjects: ➤ Rotors - Unsteady flow - Wave propagation - Blade tips - Flow distribution - Flow meters - Dynamic testing
Edition Identifiers:
- The Open Library ID: OL18657731M - OL17602478M - OL18131725M - OL15538596M
- Online Computer Library Center (OCLC) ID: 47724302
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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3Low-cost FM oscillator for capacitance type of blade tip clearance measurement system
By John P. Barranger
“Low-cost FM oscillator for capacitance type of blade tip clearance measurement system” Metadata:
- Title: ➤ Low-cost FM oscillator for capacitance type of blade tip clearance measurement system
- Author: John P. Barranger
- Language: English
- Number of Pages: Median: 12
- Publisher: ➤ Lewis Research Center - For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1987
- Publish Location: ➤ Cleveland, Ohio - [Washington, D.C.] - [Springfield, Va
“Low-cost FM oscillator for capacitance type of blade tip clearance measurement system” Subjects and Themes:
- Subjects: Blade tips - Electric Oscillators - Oscillators - Oscillators, Electric - Turbomachinery
Edition Identifiers:
- The Open Library ID: OL19003067M - OL16371511M - OL18029136M - OL15275199M
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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4Evaluation of a doubly-swept blade tip for rotorcraft noise reduction
By Brian E. Wake
“Evaluation of a doubly-swept blade tip for rotorcraft noise reduction” Metadata:
- Title: ➤ Evaluation of a doubly-swept blade tip for rotorcraft noise reduction
- Author: Brian E. Wake
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1992
- Publish Location: [Springfield, Va - Hampton, Va
“Evaluation of a doubly-swept blade tip for rotorcraft noise reduction” Subjects and Themes:
- Subjects: ➤ Rotary wings - Aeroacoustics - Blade tips - Blade slap noise - Aircraft noise - Sweep effect - Rotary wing aircraft - Blade-vortex interaction - Noise reduction - Euler equations of motion - Acoustic properties
Edition Identifiers:
- The Open Library ID: OL15413638M - OL18081154M - OL17017557M
- Online Computer Library Center (OCLC) ID: 33411839
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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5The three dimensional flow field at the exit of an axial-flow turbine rotor
By B. Lakshminarayana
“The three dimensional flow field at the exit of an axial-flow turbine rotor” Metadata:
- Title: ➤ The three dimensional flow field at the exit of an axial-flow turbine rotor
- Author: B. Lakshminarayana
- Language: English
- Publisher: ➤ National Technical Information Service [distributor - National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1998
- Publish Location: ➤ [Cleveland, Ohio] - Springfield, VA
“The three dimensional flow field at the exit of an axial-flow turbine rotor” Subjects and Themes:
- Subjects: ➤ Viscous flow - Fluid dynamics - Boundary layer separation - Blade tips - Three dimensional flow - Spatial resolution - Axial flow turbines - Vorticity - Wakes
Edition Identifiers:
- The Open Library ID: OL15544533M - OL17597293M
- Online Computer Library Center (OCLC) ID: 41899970
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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6Ramp-integration technique for capacitance-type blade-tip clearance measurement
By Garimella R. Sarma
“Ramp-integration technique for capacitance-type blade-tip clearance measurement” Metadata:
- Title: ➤ Ramp-integration technique for capacitance-type blade-tip clearance measurement
- Author: Garimella R. Sarma
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1986
- Publish Location: [Cleveland, Ohio
“Ramp-integration technique for capacitance-type blade-tip clearance measurement” Subjects and Themes:
- Subjects: ➤ Capacitance switches - Blade tips - Switched capacitor circuits - Turbomachines - Measuring instruments - Turbomachinery - Clearances
Edition Identifiers:
- The Open Library ID: OL18289831M - OL16151211M
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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7Experimental 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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8A reduced model for prediction of thermal and rotational effects on turbine tip clearance
By Javier A. Kypuros
“A reduced model for prediction of thermal and rotational effects on turbine tip clearance” Metadata:
- Title: ➤ A reduced model for prediction of thermal and rotational effects on turbine tip clearance
- Author: Javier A. Kypuros
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2003
- Publish Location: [Cleveland, Ohio]
“A reduced model for prediction of thermal and rotational effects on turbine tip clearance” Subjects and Themes:
- Subjects: ➤ Blade tips - Clearances - Dynamic models - Mathematical models - Scale models - Temperature effects - Turbine blades
Edition Identifiers:
- The Open Library ID: OL17722590M - OL17635033M
- Online Computer Library Center (OCLC) ID: 58833954
Access and General Info:
- First Year Published: 2003
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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9Analysis of gas turbine rotor blade tip and shroud heat transfer
By A. A. Ameri
“Analysis of gas turbine rotor blade tip and shroud heat transfer” Metadata:
- Title: ➤ Analysis of gas turbine rotor blade tip and shroud heat transfer
- Author: A. A. Ameri
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996 - 1998
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Analysis of gas turbine rotor blade tip and shroud heat transfer” Subjects and Themes:
- Subjects: ➤ Gas turbines - Heat transfer - Blade tips - Shrouds - Boundary layer thickness - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL17593523M - OL15505238M
- Online Computer Library Center (OCLC) ID: 41970343
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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10Effects of tip clearance and casing recess on heat transfer and stage efficiency in axial turbines
By A. A. Ameri
“Effects of tip clearance and casing recess on heat transfer and stage efficiency in axial turbines” Metadata:
- Title: ➤ Effects of tip clearance and casing recess on heat transfer and stage efficiency in axial turbines
- Author: A. A. Ameri
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1998
- Publish Location: ➤ [Cleveland, Ohio] - [Springfield, Va
“Effects of tip clearance and casing recess on heat transfer and stage efficiency in axial turbines” Subjects and Themes:
- Subjects: ➤ Gas turbines - Heat transfer - Recesses - Blade tips - Axial flow turbines - Clearances
Edition Identifiers:
- The Open Library ID: OL17839067M - OL15545026M
- Online Computer Library Center (OCLC) ID: 41394943
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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11The spectral and statistical properties of turbulence generated by a vortex/blade-tip interaction
By William J. Devenport
“The spectral and statistical properties of turbulence generated by a vortex/blade-tip interaction” Metadata:
- Title: ➤ The spectral and statistical properties of turbulence generated by a vortex/blade-tip interaction
- Author: William J. Devenport
- Language: English
- Publisher: ➤ Dept. of Aerospace and Ocean Engineering, Virginia Polytechnic Institute and State University - National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC - Blacksburg, VA
“The spectral and statistical properties of turbulence generated by a vortex/blade-tip interaction” Subjects and Themes:
- Subjects: ➤ Helicopters - Rotary wings - Aeroacoustics - Blade tips - Blade slap noise - Statistical distributions - Noise prediction - Blade-vortex interaction - Aerodynamic noise - Turbulent wakes - Interactional aerodynamics - Incompressible flow
Edition Identifiers:
- The Open Library ID: OL15479176M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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12Heat transfer and flow on the first stage blade tip of a power generation gas turbine
By Ronald S. Bunker
“Heat transfer and flow on the first stage blade tip of a power generation gas turbine” Metadata:
- Title: ➤ Heat transfer and flow on the first stage blade tip of a power generation gas turbine
- Author: Ronald S. Bunker
- 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]
“Heat transfer and flow on the first stage blade tip of a power generation gas turbine” Subjects and Themes:
- Subjects: ➤ Gas turbines - Heat transfer - Convective heat transfer - Blade tips - Pressure distribution - Heat transfer coefficients - Turbine blades
Edition Identifiers:
- The Open Library ID: OL15552406M
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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13Prediction of unshrouded rotor blade tip heat transfer
By A. A. Ameri
“Prediction of unshrouded rotor blade tip heat transfer” Metadata:
- Title: ➤ Prediction of unshrouded rotor blade tip heat transfer
- Author: A. A. Ameri
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Prediction of unshrouded rotor blade tip heat transfer” Subjects and Themes:
- Subjects: Heat transfer - Turbine blades - Computation - Blade tips - Computer programs
Edition Identifiers:
- The Open Library ID: OL15505241M
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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14Development of a fiber optic compressor blade sensor
By Harbans Singh Dhadwal
“Development of a fiber optic compressor blade sensor” Metadata:
- Title: ➤ Development of a fiber optic compressor blade sensor
- Author: Harbans Singh Dhadwal
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Development of a fiber optic compressor blade sensor” Subjects and Themes:
- Subjects: ➤ Measuring instruments - Light beams - Blade tips - Sensors - Fiber optics - Compressor blades
Edition Identifiers:
- The Open Library ID: OL15419788M
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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15Optical measurement of unducted fan flutter
By Anatole P Kurkov
“Optical measurement of unducted fan flutter” Metadata:
- Title: ➤ Optical measurement of unducted fan flutter
- Author: Anatole P Kurkov
- Language: English
- Publisher: ➤ NASA - National Technical Information Service, distributor
- Publish Date: 1991
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Optical measurement of unducted fan flutter” Subjects and Themes:
- Subjects: ➤ Optical measurement - Nonlinearity - Blade tips - Counter rotation - Rotors - Vibration mode - Aeroelasticity - Flutter - Centrifugal force
Edition Identifiers:
- The Open Library ID: OL15404767M
Author's Alternative Names:
"Anatole P. Kurkov"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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16Euler solutions to nonlinear acoustics of non-lifting hovering rotor blades
By J. D. Baeder
“Euler solutions to nonlinear acoustics of non-lifting hovering rotor blades” Metadata:
- Title: ➤ Euler solutions to nonlinear acoustics of non-lifting hovering rotor blades
- Author: J. D. Baeder
- Language: English
- Publisher: ➤ US Army Aviation Systems Command, Aviation Research and Technology Activity - National Aeronautics and Space Administration, Ames Research Center - For sale by the National Technical Information Service, distributor
- Publish Date: 1991
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Euler solutions to nonlinear acoustics of non-lifting hovering rotor blades” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Rotor aerodynamics - Nonlinearity - Blade tips - Rotor blades (Turbomachinery) - Stability - Hovering - Acoustic properties - Euler equations of motion
Edition Identifiers:
- The Open Library ID: OL17114268M
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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17An examination of the aerodynamic moment on rotor blade tips using flight test data and analysis
By Thomas H. Maier
“An examination of the aerodynamic moment on rotor blade tips using flight test data and analysis” Metadata:
- Title: ➤ An examination of the aerodynamic moment on rotor blade tips using flight test data and analysis
- Author: Thomas H. Maier
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - US Army Aviation and Troop Command - National Technical Information Service, distributor
- Publish Date: 1993
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“An examination of the aerodynamic moment on rotor blade tips using flight test data and analysis” Subjects and Themes:
- Subjects: Pitching moments - Rotary wings - Rotor aerodynamics - Blade tips - Torsion
Edition Identifiers:
- The Open Library ID: OL15415725M
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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18Aerodynamic limitations of the UH-60A rotor
By Colin P. Coleman
“Aerodynamic limitations of the UH-60A rotor” Metadata:
- Title: ➤ Aerodynamic limitations of the UH-60A rotor
- Author: Colin P. Coleman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Aerodynamic limitations of the UH-60A rotor” Subjects and Themes:
- Subjects: ➤ Pitching moments - UH-60A helicopter - Blade tips - Aerodynamic loads - Rotors - Supercritical flow - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL15498141M
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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19Blade tip rubbing stress prediction
By Davis, Gary A.
“Blade tip rubbing stress prediction” Metadata:
- Title: ➤ Blade tip rubbing stress prediction
- Author: Davis, Gary A.
- Language: English
- Publisher: ➤ Rockwell International, Rocketdyne Division
- Publish Date: 1991
- Publish Location: Canoga Park, Calif
“Blade tip rubbing stress prediction” Subjects and Themes:
- Subjects: ➤ Blade tips - Kinetic friction - Prediction analysis techniques - Space shuttle main engine - Stress analysis - Turbine blades - Turbine pumps
Edition Identifiers:
- The Open Library ID: OL16133029M
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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Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Wind turbine
in turbulent winds; and a lower blade speed ratio, which lowers blade bending stresses. Straight, V, or curved blades may be used. These are drag-type
Unequal rotor lift distribution
effect where the blades of a helicopter rotor generate more lift at the rotor tips than at the rotor hub. A helicopter rotor blade is an airfoil, which
Jet engine performance
past the blade tips generates entropy and reduces the efficiency of the compressor and turbine. Interlocking shrouds are present on the tips of low pressure
Propeller
and trailing tips of the sections depicts the expanded blade outline. The pitch diagram shows variation of pitch with radius from root to tip. The transverse
Stiletto
slender blade and needle-like point, primarily intended as a thrusting and stabbing weapon. The stiletto blade's narrow cross-section and acuminated tip (that
Wingtip device
blade tip profile C-130J Super Hercules showing scimitar propellers with raked tips Detail view of the wingtip device on a wind turbine rotor-blade Ceiling
Propfan
combined with the rotational speed of the propeller blade tips (together known as the helical tip speed) will again result in wave drag problems. For
Vortex ring state
a rotationally symmetrical form over the tips of the blades, supported by a laminar flow over the blade tips, and a countering upflow of air outside and
Ducted fan
the fan and closely fits the blade tips. It must be made rigid enough not to distort under flight loads nor touch the blades as they turn. The duct performs
Blade
A blade is the sharp, cutting portion of a tool, weapon, or machine, specifically designed to puncture, chop, slice, or scrape surfaces or materials.