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Proceedings Papers
Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery
Aircraft Engine
Investigation of Vapor-Phase Lubrication in a Gas Turbine Engine
GT 1997; V001T01A001https://doi.org/10.1115/97-GT-003
Topics:
Gas turbines
,
Lubrication
,
Vapors
,
Bearings
,
Engines
,
Temperature
,
Aircraft
,
Industrial lubrication systems
,
Lubricants
,
Weight (Mass)
Getting to Problem Definition
GT 1997; V001T01A002https://doi.org/10.1115/97-GT-033
Topics:
Aircraft
,
Design
,
Gas turbines
,
Hardware
,
Teams
Ideal Power Output — An Alternative Aircraft Engine Performance Comparator
GT 1997; V001T01A004https://doi.org/10.1115/97-GT-228
Topics:
Aircraft engines
,
Cycles
,
Engines
,
Flight
,
Gas turbines
,
Pressure
,
Thrust
,
Turbofans
,
Turbojets
,
Turbomachinery
Turbine Engine Installed Performance Optimisation With a Multi-Axis Thrust Vectoring Nozzle
GT 1997; V001T01A006https://doi.org/10.1115/97-GT-258
Topics:
Gas turbines
,
Nozzles
,
Optimization
,
Thrust
,
Aircraft engines
,
Computers
,
Engines
,
Flight
,
Fluids
,
Fuel consumption
Future Material Needs for Low Emissions Gas Turbines
GT 1997; V001T01A007https://doi.org/10.1115/97-GT-262
Topics:
Emissions
,
Gas turbines
,
Materials science
,
Pressure
,
Combustion chambers
,
Engines
,
Fuels
,
High temperature
,
High temperature materials
,
Materials properties
Variable Flow Turbofan Engine for an HSCT Application
GT 1997; V001T01A009https://doi.org/10.1115/97-GT-264
Topics:
Engines
,
Flow (Dynamics)
,
Turbofans
,
Geometry
,
Thrust
,
Aircraft propulsion
,
Compressors
,
Design
,
Flight
,
Guide vanes
Research of a High Thrust-to-Weight Ratio Small Turbofan Engine
GT 1997; V001T01A010https://doi.org/10.1115/97-GT-289
Topics:
Engines
,
Thrust
,
Turbofans
,
Weight (Mass)
,
Aircraft
,
Defense industry
,
Design
,
Industrial research
Effects of Engine Aging on Aircraft NOx Emissions
GT 1997; V001T01A011https://doi.org/10.1115/97-GT-386
Topics:
Aircraft
,
Emissions
,
Engines
,
Nitrogen oxides
,
Combustion chambers
,
Cycles
,
Flow (Dynamics)
,
Compressors
,
Turbines
,
Fuel consumption
The Development of the Whittle Turbojet
GT 1997; V001T01A012https://doi.org/10.1115/97-GT-528
Topics:
Turbojets
,
Compressors
,
Design
,
Aircraft propulsion
,
Boilers
,
Combustion
,
Engine design
,
Jets
,
Mechanical engineering
,
Pressure
Marine
Allison 501-K17 SSGTGS Technical Directive Experience
GT 1997; V001T02A001https://doi.org/10.1115/97-GT-169
Topics:
Electricity (Physics)
,
Gas turbines
,
Generators
,
Maintainability
,
Missiles
,
Navy
,
Reliability
,
Seas
,
Ships
,
Systems engineering
Research Into the Drive Transition of Combined Diesel or Gas Turbine Plant
GT 1997; V001T02A003https://doi.org/10.1115/97-GT-171
Topics:
Diesel
,
Gas turbines
,
Torque
,
Diesel engines
,
Fuels
,
Computer simulation
,
Engines
,
Hydraulic couplings
Back Fitting Maintainability Into a Gas Turbine Generator Set
GT 1997; V001T02A005https://doi.org/10.1115/97-GT-178
Topics:
Fittings
,
Gas turbines
,
Generators
,
Maintainability
,
Navy
,
Ships
,
Fluids
Alternative Starting Methods for Shipboard Gas Turbine Generators
GT 1997; V001T02A006https://doi.org/10.1115/97-GT-251
Topics:
Gas turbines
,
Generators
,
Ships
,
Engines
,
High pressure (Physics)
,
Machinery
,
Navy
,
Pipes
,
Valves
A Mechanical Start System for U. S. Navy Destroyer Generator Sets
GT 1997; V001T02A007https://doi.org/10.1115/97-GT-252
Topics:
Generators
,
Navy
,
Mechanical drives
,
High pressure (Physics)
,
Engines
,
Turbines
,
Compressed air
,
Construction
,
Gas turbines
,
Maintenance
A Steam-Augmented Gas Turbine With Reheat Combustor for Surface Ships
GT 1997; V001T02A009https://doi.org/10.1115/97-GT-254
Topics:
Combustion chambers
,
Gas turbines
,
Ships
,
Steam
,
Engines
,
Temperature
,
Simulation
,
Air flow
,
Flow (Dynamics)
,
Fuels
Simulation of Transient Load Behaviour of Gas Turbines in High Speed Marine Applications
GT 1997; V001T02A010https://doi.org/10.1115/97-GT-457
Topics:
Gas turbines
,
Simulation
,
Stress
,
Transients (Dynamics)
,
Torque
,
Design
,
Seas
,
Temperature
,
Turbines
,
Vessels
WR-21 Recuperator Core Test
GT 1997; V001T02A012https://doi.org/10.1115/97-GT-514
Topics:
Aerospace industry
,
Cycles
,
Design
,
Engines
,
Exhaust systems
,
Fuel consumption
,
Fuels
,
Gas turbines
,
Heat
,
Instrumentation
Unique Reverse and Maneuvering Features of the AOE-6 Reverse Reduction Gear
GT 1997; V001T02A013https://doi.org/10.1115/97-GT-515
Topics:
Gears
,
Ships
,
Rotors
,
Stators
,
Warfare
,
Circuits
,
Design
,
Displacement
,
Fluid dynamics
,
Gas turbines
Turbomachinery
Experimental Investigation of Stepped Tip Gap Effects on the Performance of a Transonic Axial-Flow Compressor Rotor
GT 1997; V001T03A002https://doi.org/10.1115/97-GT-007
Topics:
Axial flow
,
Compressors
,
Rotors
,
Clearances (Engineering)
,
Flow (Dynamics)
,
Design
,
Engineers
,
Inlet guide vanes
,
Pressure
Breakdown of Tip Leakage Vortices in Compressors at Flow Conditions Close to Stall
GT 1997; V001T03A004https://doi.org/10.1115/97-GT-041
Topics:
Compressors
,
Flow (Dynamics)
,
Leakage
,
Vortices
,
Rotors
,
Computation
,
Stability
,
Stall inception
,
Visualization
Effects of Stream Surface Inclination on Tip Leakage Flow Fields in Compressor Rotors
GT 1997; V001T03A006https://doi.org/10.1115/97-GT-043
Topics:
Compressors
,
Leakage flows
,
Rotors
,
Vortices
,
Flow (Dynamics)
,
Axial flow
,
Leakage
,
Boundary layers
,
Airfoils
,
Blades
High Freestream Turbulence Simulation in a Scaled-Up Turbine Vane Passage
GT 1997; V001T03A009https://doi.org/10.1115/97-GT-051
Topics:
Simulation
,
Turbines
,
Turbulence
,
Generators
,
Blades
,
Stators
,
Boundary layers
,
Computational fluid dynamics
,
Flow (Dynamics)
,
Gas turbines
The Effect of Tip Clearance on the Development of Loss Behind a Rotor and a Subsequent Nozzle
GT 1997; V001T03A011https://doi.org/10.1115/97-GT-053
Topics:
Clearances (Engineering)
,
Nozzles
,
Rotors
,
Flow (Dynamics)
,
Blades
,
Shapes
,
Leakage flows
,
Machinery
,
Cascades (Fluid dynamics)
,
Design
Characteristics of a Turbine Cascade at Low Reynolds Numbers
GT 1997; V001T03A012https://doi.org/10.1115/97-GT-054
Topics:
Cascades (Fluid dynamics)
,
Reynolds number
,
Turbines
,
Pressure
,
Airfoils
,
Wakes
,
Separation (Technology)
,
Blades
,
Boundary layers
,
Bubbles
Numerical Analysis of Transonic Compressor Rotor Flow Near Stall Points
GT 1997; V001T03A014https://doi.org/10.1115/97-GT-068
Topics:
Compressors
,
Flow (Dynamics)
,
Numerical analysis
,
Rotors
,
Clearances (Engineering)
,
Design
,
Shock (Mechanics)
,
Surges
,
Failure
,
Geometry
A Numerical Investigation of Transonic Axial Compressor Rotor Flow Using a Low Reynolds Number k-ε Turbulence Model
GT 1997; V001T03A017https://doi.org/10.1115/97-GT-082
Topics:
Compressors
,
Flow (Dynamics)
,
Reynolds number
,
Rotors
,
Turbulence
,
Design
,
NASA
,
Computer simulation
,
Lasers
,
Navier-Stokes equations
Numerical Prediction of Trailing Edge Wake Shedding
GT 1997; V001T03A020https://doi.org/10.1115/97-GT-089
Topics:
Algebra
,
Blades
,
Navier-Stokes equations
,
Stators
,
Turbines
,
Turbulence
,
Vortex shedding
,
Wakes
Numerical Simulation of the Flow Through the Rotor of a Radial Inflow Turbine
GT 1997; V001T03A021https://doi.org/10.1115/97-GT-090
Topics:
Computer simulation
,
Flow (Dynamics)
,
Inflow
,
Rotors
,
Turbines
,
Blades
,
Clearances (Engineering)
,
Turbulence
,
Viscous flow
,
Design
Axial Compressor Stage Analysis Through a Multi-Block 3-D Navier-Stokes Solution Method
GT 1997; V001T03A024https://doi.org/10.1115/97-GT-093
Topics:
Compressors
,
Flow (Dynamics)
,
Rotors
,
Stators
,
Blades
,
Clearances (Engineering)
,
Modeling
,
Physics
,
Pressure
,
Scalars
Prediction of 3D-Unsteady Flow in an Air Turbine and a Transonic Compressor Including Blade Gap Flow and Blade Row Interaction
GT 1997; V001T03A025https://doi.org/10.1115/97-GT-094
Topics:
Blades
,
Compressors
,
Flow (Dynamics)
,
Turbines
,
Stators
,
Axial flow
,
Computation
,
Inlet guide vanes
,
Navier-Stokes equations
,
Rotors
Origins of Loss Within a Multistage Turbine Environment Under Conditions of Partial Admission
GT 1997; V001T03A027https://doi.org/10.1115/97-GT-096
Topics:
Turbines
,
Pressure
,
Axial flow
,
Bending (Stress)
,
Blades
,
Computational fluid dynamics
,
Cycles
,
Design
,
Design methodology
,
Flow (Dynamics)
Engine Representative Discharge Coefficients Measured in an Annular Nozzle Guide Vane Cascade
GT 1997; V001T03A030https://doi.org/10.1115/97-GT-099
Topics:
Cascades (Fluid dynamics)
,
Discharge coefficient
,
Engines
,
Nozzle guide vanes
,
Coolants
,
Flow (Dynamics)
,
Aircraft engines
,
Film cooling
,
Blades
,
Cooling
Analysis of Separated Flows Inside an Annular Compressor Cascade Using a Low-Re-Number k-ϵ and an Algebraic Reynolds-Stress-Model
GT 1997; V001T03A032https://doi.org/10.1115/97-GT-132
Topics:
Algebra
,
Cascades (Fluid dynamics)
,
Compressors
,
Flow (Dynamics)
,
Stress
,
Turbulence
,
Anisotropy
,
Inflow
,
Pressure
,
Separation (Technology)
The Performance of a Centrifugal Compressor With High Inlet Prewhirl
GT 1997; V001T03A033https://doi.org/10.1115/97-GT-182
Topics:
Compressors
,
Pressure
,
Surges
,
Flow (Dynamics)
,
Geometry
,
Design
,
Ducts
,
Generators
,
Impellers
,
Inlet guide vanes
An Analysis Method for Multistage Transonic Turbines With Coolant Mass Flow Addition
GT 1997; V001T03A034https://doi.org/10.1115/97-GT-183
Topics:
Coolants
,
Flow (Dynamics)
,
Turbines
,
Blades
,
Cooling
,
Algorithms
,
Entropy
,
Finite volume methods
,
Fluid dynamics
,
Gas turbines
Numerical Flow Analysis in a Subsonic Vaned Radial Diffuser With Leading Edge Redesign
GT 1997; V001T03A035https://doi.org/10.1115/97-GT-185
Topics:
Diffusers
,
Flow (Dynamics)
,
Pressure
,
Blades
,
Compressors
,
Computer software
,
Design
,
Geometry
Investigation of Tip Leakage Effects in Transonic Flow Using a Parallel Unstructured Navier-Stokes Code
GT 1997; V001T03A036https://doi.org/10.1115/97-GT-202
Topics:
Leakage
,
Transonic flow
,
Flow (Dynamics)
,
Blades
,
Boundary layers
,
Cascades (Fluid dynamics)
,
Turbine blades
,
Engines
,
Flat plates
,
Inflow
Blade Film Cooling by Underexpanded Transonic Jet Layers
GT 1997; V001T03A042https://doi.org/10.1115/97-GT-246
Topics:
Blades
,
Film cooling
,
Jets
,
Cascades (Fluid dynamics)
,
Coolants
,
Flow (Dynamics)
,
Turbines
,
Chords (Trusses)
,
Cooling
,
Temperature
Influence of a Mixing-Jet on Film Cooling
GT 1997; V001T03A043https://doi.org/10.1115/97-GT-247
A Study of Acoustic Resonance in a Low-Speed Multistage Compressor
GT 1997; V001T03A045https://doi.org/10.1115/97-GT-259
Topics:
Acoustics
,
Compressors
,
Resonance
,
Flow (Dynamics)
,
Pressure
,
Compression
,
Signals
,
Stators
The Turbulence That Matters
GT 1997; V001T03A046https://doi.org/10.1115/97-GT-274
Throughflow Design Using an Automatic Optimisation Strategy
GT 1997; V001T03A047https://doi.org/10.1115/97-GT-294
Topics:
Design
,
Optimization
,
Flow (Dynamics)
,
Geometry
,
High pressure (Physics)
,
Steam turbines
,
Turbines
Inverse Design of Turbomachinery Blading for Arbitrary Blade Thickness in Three-Dimensional Transonic Flow
GT 1997; V001T03A048https://doi.org/10.1115/97-GT-295
Topics:
Blades
,
Design
,
Transonic flow
,
Turbomachinery
,
Vortices
,
Pressure
,
Shock (Mechanics)
,
Suction
,
Boundary-value problems
,
Density
Laser Anemometer Measurements of the Flow Field in a 4:1 Pressure Ratio Centrifugal Impeller
GT 1997; V001T03A049https://doi.org/10.1115/97-GT-342
Topics:
Flow (Dynamics)
,
Impellers
,
Lasers
,
Pressure
,
Blades
,
Clearances (Engineering)
,
Suction
,
Vaneless diffusers
,
Chords (Trusses)
,
Computational fluid dynamics
Detailed Off Design Flow Measurements in a Centrifugal Compressor Vaned Diffuser
GT 1997; V001T03A050https://doi.org/10.1115/97-GT-343
Topics:
Compressors
,
Design
,
Diffusers
,
Flow measurement
,
Flow (Dynamics)
,
Wakes
,
Blades
,
Impellers
,
Turbulence
,
Vaneless diffusers
Aerodynamic Modeling of Multistage Compressor Flowfields: Part 1 — Analysis of Rotor/Stator/Rotor Aerodynamic Interaction
GT 1997; V001T03A051https://doi.org/10.1115/97-GT-344
Topics:
Compressors
,
Modeling
,
Rotors
,
Stators
,
Flow (Dynamics)
,
Axial flow
,
Computational fluid dynamics
,
Blades
,
Density
,
Design
Aerodynamic Modeling of Multistage Compressor Flowfields: Part 2 — Modeling Deterministic Stresses
GT 1997; V001T03A052https://doi.org/10.1115/97-GT-345
Topics:
Compressors
,
Modeling
,
Stress
,
Blades
,
Wakes
,
Flow (Dynamics)
,
Axial flow
,
Design
,
Rotors
,
Clearances (Engineering)
The Effect of Hub Leakage Flow on Two High Speed Axial Flow Compressor Rotors
GT 1997; V001T03A053https://doi.org/10.1115/97-GT-346
Topics:
Axial flow
,
Leakage flows
,
Rotors
,
Engineering simulation
,
Flow (Dynamics)
,
Simulation
,
Computational fluid dynamics
,
Computer simulation
,
Leakage
,
Pressure
A Practical Compressor Casing Treatment
GT 1997; V001T03A054https://doi.org/10.1115/97-GT-375
Topics:
Compressors
,
Flow (Dynamics)
,
Pressure
,
Blades
,
Design
,
Dynamics (Mechanics)
,
Honeycomb structures
,
Jets
,
Momentum
,
Suction
Grid Dependency Study for the NASA Rotor 37 Compressor Blade
GT 1997; V001T03A056https://doi.org/10.1115/97-GT-384
Topics:
Blades
,
Compressors
,
NASA
,
Rotors
,
Density
,
Turbulence
,
Boundary-value problems
,
Modeling
,
Pressure
,
Shear (Mechanics)
On the Design Criteria for Suppression of Secondary Flows in Centrifugal and Mixed Flow Impellers
GT 1997; V001T03A058https://doi.org/10.1115/97-GT-393
Topics:
Design
,
Flow (Dynamics)
,
Impellers
,
Blades
,
Compressor impellers
,
Pressure
,
Centrifugal pumps
,
Compressors
,
Design methodology
,
Pumps
Blockage Development in a Transonic, Axial Compressor Rotor
GT 1997; V001T03A059https://doi.org/10.1115/97-GT-394
Topics:
Compressors
,
Rotors
,
Flow (Dynamics)
,
Shock (Mechanics)
,
Boundary layers
,
Axial flow
,
Blades
,
Clearances (Engineering)
,
Design
,
Lasers
Prediction of the Becalmed Region for LP Turbine Profile Design
GT 1997; V001T03A060https://doi.org/10.1115/97-GT-398
Topics:
Design
,
Turbines
,
Boundary layers
,
Turbulence
,
Separation (Technology)
,
Turbine blades
,
Wakes
,
Entropy
,
Flow (Dynamics)
,
Reynolds number
Modeling Unsteady Boundary Layer Transition on a Curved Plate Under Periodic Unsteady Flow Conditions: Aerodynamic and Heat Transfer Investigations
GT 1997; V001T03A061https://doi.org/10.1115/97-GT-399
Topics:
Boundary layers
,
Heat transfer
,
Modeling
,
Unsteady flow
,
Turbulence
,
Wakes
,
Heat transfer coefficients
,
Pressure gradient
Inner Workings of Aerodynamic Sweep
GT 1997; V001T03A062https://doi.org/10.1115/97-GT-401
Topics:
Axial flow
,
Blades
,
Boundary layers
,
Clearances (Engineering)
,
Compression
,
Design
,
Diffusion (Physics)
,
Rotors
,
Shock (Mechanics)
,
Stability
A Shock Loss Model for Supersonic Compressor Cascades
GT 1997; V001T03A065https://doi.org/10.1115/97-GT-405
Topics:
Compressors
,
Shock (Mechanics)
,
Mach number
,
Airfoils
,
Boundary layers
,
Cascades (Fluid dynamics)
,
Compression
,
Flow (Dynamics)
,
Fluid mechanics
,
Geometry
Viscous Throughflow Modelling of Axial Compressor Bladerows Using a Tangential Blade Force Hypothesis
GT 1997; V001T03A068https://doi.org/10.1115/97-GT-415
Topics:
Blades
,
Compressors
,
Modeling
,
Design
,
Flow (Dynamics)
,
Annulus
,
Boundary layers
,
Clearances (Engineering)
,
Computational fluid dynamics
,
Pressure
A Navier-Stokes Inverse Method Based on a Moving Blade Wall Strategy
GT 1997; V001T03A069https://doi.org/10.1115/97-GT-416
Topics:
Blades
,
Compressors
,
Computation
,
Design
,
Pressure
,
Transpiration
,
Flow (Dynamics)
,
Geometry
,
Navier-Stokes equations
,
Resolution (Optics)
Numerical Analysis of Two-Dimensional Compressible Viscous Flow in Turbomachinery Cascades Using an Improved k-ε Turbulence Model
GT 1997; V001T03A070https://doi.org/10.1115/97-GT-417
Topics:
Numerical analysis
,
Turbomachinery
,
Turbulence
,
Viscous flow
,
Shock (Mechanics)
,
Blades
,
Flow (Dynamics)
,
Reynolds number
,
Boundary layers
,
Compressors
A Parallel Unstructured Turbomachinery Code
GT 1997; V001T03A071https://doi.org/10.1115/97-GT-418
Design of New Three Stage Low Pressure Turbine for the BMW Rolls-Royce BR715 Turbofan Engine
GT 1997; V001T03A072https://doi.org/10.1115/97-GT-419
Topics:
Design
,
Engines
,
Pressure
,
Turbines
,
Turbofans
,
Thrust
,
Airfoils
,
Design engineering
,
High pressure (Physics)
,
Jets
Study of a Low Aspect Ratio Low Pressure Turbine Nozzle Guide Vane With High Outer Annulus Wall Slope
GT 1997; V001T03A073https://doi.org/10.1115/97-GT-420
Topics:
Annulus
,
Nozzle guide vanes
,
Pressure
,
Turbines
,
Rotors
,
Computational fluid dynamics
,
Flow (Dynamics)
,
Chords (Trusses)
,
Fluctuations (Physics)
,
Vortices
Three-Dimensional Navier-Stokes Analysis of Turbine Rotor and Tip-Leakage Flowfield
GT 1997; V001T03A074https://doi.org/10.1115/97-GT-421
Topics:
Leakage
,
Rotors
,
Turbines
,
Flow (Dynamics)
,
Turbulence
,
Blades
,
Clearances (Engineering)
,
Geometry
,
Mesh generation
,
Rotation
Influence of 3D Hot Streaks on Turbine Heat Transfer
GT 1997; V001T03A075https://doi.org/10.1115/97-GT-422
Topics:
Heat transfer
,
Turbines
,
Combustion chambers
,
Engineering simulation
,
Pressure
,
Simulation
,
Airfoils
,
Blades
,
Combustion
,
Cooling
Entropy Generation Measurement in a Laminar Turbine Blade Boundary-Layer
GT 1997; V001T03A076https://doi.org/10.1115/97-GT-450
Topics:
Boundary layers
,
Entropy
,
Turbine blades
,
Blades
,
Heat transfer
,
Temperature
,
Valves
,
Air flow
,
Cascades (Fluid dynamics)
,
Ceramics
Studies on Wake-Disturbed Boundary Layers Under the Influences of Favorable Pressure Gradient and Free-Stream Turbulence: Part I — Experimetal Setup and Discussions on Transition Model
GT 1997; V001T03A077https://doi.org/10.1115/97-GT-451
Topics:
Boundary layers
,
Pressure gradient
,
Turbulence
,
Wakes
,
Flat plates
,
Generators
,
Heat transfer
,
Probes
,
Stainless steel
,
Wheels
Studies on Wake-Disturbed Boundary Layers Under the Influences of Favorable Pressure Gradient and Free-Stream Turbulence: Part II — Effect of Free-Stream Turbulence
GT 1997; V001T03A078https://doi.org/10.1115/97-GT-452
Topics:
Boundary layers
,
Pressure gradient
,
Turbulence
,
Wakes
,
Heat transfer
,
Probes
,
Shapes
,
Wire
An Experimental Investigation of Transition as Applied to Low Pressure Turbine Suction Surface Flows
GT 1997; V001T03A081https://doi.org/10.1115/97-GT-455
Topics:
Flow (Dynamics)
,
Pressure
,
Suction
,
Turbines
,
Separation (Technology)
,
Boundary layers
,
Bubbles
,
Reynolds number
,
Shear (Mechanics)
,
Airfoils
The Use of Cyclic Variations in Strut Stagger to Reduce Coupled Blade-Vane-Strut-Pylon Interaction and System Losses
GT 1997; V001T03A086https://doi.org/10.1115/97-GT-470
Topics:
Blades
,
Struts (Engineering)
,
Engines
,
Flow (Dynamics)
,
Actuators
,
Computational fluid dynamics
,
Design
,
Dimensions
,
Disks
,
Guide vanes
Effect of a Mismatch Between the Buttons of Variable Stator Vanes and the Flowpath in a Highly Loaded Transonic Compressor Stage
GT 1997; V001T03A087https://doi.org/10.1115/97-GT-471
Topics:
Compressors
,
Stators
,
Flow (Dynamics)
,
Computation
,
Annulus
,
Corners (Structural elements)
,
Defense industry
,
Flow separation
,
Flow turning
,
Geometry
Pressure Recovery in Low Solidity Vaned Diffusers for Centrifugal Compressors
GT 1997; V001T03A088https://doi.org/10.1115/97-GT-472
Topics:
Compressors
,
Diffusers
,
Pressure
,
Bearings
,
Impellers
The Unsteady Pressure Field Over a Turbine Blade Surface: Visualisation and Interpretation of Experimental Data
GT 1997; V001T03A090https://doi.org/10.1115/97-GT-474
Topics:
Pressure
,
Turbine blades
,
Visualization
,
Blades
,
Rotors
,
Fluctuations (Physics)
,
Wakes
,
Cycles
,
Flow (Dynamics)
,
Nozzle guide vanes
Development of a High Pressure Ratio Centrifugal Compressor for 300kW-Class Ceramic Gas Turbine
GT 1997; V001T03A093https://doi.org/10.1115/97-GT-480
Topics:
Ceramics
,
Compressors
,
Gas turbines
,
High pressure (Physics)
,
Turbines
,
Diffusers
,
Engines
,
Flow (Dynamics)
,
Impellers
,
Industrial research
Experimental and Numerical Analysis of Compressor Inlet Volutes
GT 1997; V001T03A094https://doi.org/10.1115/97-GT-481
Topics:
Compressors
,
Numerical analysis
,
Flow (Dynamics)
,
Geometry
,
Turbulence
,
Compressor impellers
,
Computation
,
Computers
,
Design
,
Mach number
Experimental and Numerical Investigation of Boundary-Layer and Wake Development in a Transonic Turbine Cascade
GT 1997; V001T03A095https://doi.org/10.1115/97-GT-483
Topics:
Boundary layers
,
Cascades (Fluid dynamics)
,
Turbines
,
Wakes
,
Pressure
,
Blades
,
Computation
,
Flow (Dynamics)
,
Shock (Mechanics)
,
Flow separation
Design Modification of Rotor 67 by 3D Inverse Method — Inviscid-Flow Limit
GT 1997; V001T03A096https://doi.org/10.1115/97-GT-484
Topics:
Design
,
Inviscid flow
,
Rotors
,
Blades
,
Pressure
,
Shapes
,
Shock (Mechanics)
,
Geometry
Wake Decay: Effect of Freestream Swirl
GT 1997; V001T03A097https://doi.org/10.1115/97-GT-495
Topics:
Wakes
,
Rotors
,
Cascades (Fluid dynamics)
,
Stators
,
Acoustics
,
Blades
,
Chords (Trusses)
,
Fluids
,
Noise (Sound)
,
Rotating blades
Effects of Stator Indexing on Performance in a Low Speed Multistage Axial Compressor
GT 1997; V001T03A098https://doi.org/10.1115/97-GT-496
Topics:
Compressors
,
Indexing (Machining)
,
Stators
,
Blades
,
Manufacturing
,
Pressure
,
NASA
,
Testing
,
Wakes
The Aerodynamics of Trailing-Edge-Cooled Transonic Turbine Blades: Part 1 — Experimental Approach
GT 1997; V001T03A101https://doi.org/10.1115/97-GT-518
Topics:
Aerodynamics
,
Boundary layers
,
Cavities
,
Coolants
,
Flat plates
,
Flow (Dynamics)
,
Mach number
,
Pressure
,
Shock (Mechanics)
,
Temperature
The Influence of Film Cooling on the Efficiency of an Annular Nozzle Guide Vane Cascade
GT 1997; V001T03A104https://doi.org/10.1115/97-GT-521
Topics:
Cascades (Fluid dynamics)
,
Film cooling
,
Nozzle guide vanes
,
Coolants
,
Design
,
Momentum
,
Engines
,
Probes
,
Airfoils
,
Computational fluid dynamics
The Influence of Film-Cooling on the Aerodynamic Performance of a Turbine Nozzle Guide Vane
GT 1997; V001T03A105https://doi.org/10.1115/97-GT-522
Topics:
Film cooling
,
Nozzle guide vanes
,
Turbines
,
Flow (Dynamics)
,
Coolants
,
Blades
,
Cooling
,
Pressure
,
Carbon dioxide
,
Momentum
Flow Field Measurements on a Large Scale Turbine Cascade With Leading Edge Film Cooling by Two Rows of Holes
GT 1997; V001T03A107https://doi.org/10.1115/97-GT-524
Topics:
Cascades (Fluid dynamics)
,
Film cooling
,
Flow (Dynamics)
,
Turbines
,
Pressure
,
Vortices
,
Suction
,
Kidney
,
Blades
,
Bubbles
Aspirated Compressors
GT 1997; V001T03A108https://doi.org/10.1115/97-GT-525
Topics:
Compressors
,
Suction
,
Blades
,
Rotors
,
Boundary layers
,
Flow (Dynamics)
,
Pressure
,
Compression
,
Fluids
,
Engines
A Study of Spike and Modal Stall Phenomena in a Low-Speed Axial Compressor
GT 1997; V001T03A109https://doi.org/10.1115/97-GT-526
Topics:
Compressors
,
Flow (Dynamics)
,
Stall inception
,
Compression
,
Rotors
,
Stability
Wake Recovery Performance Benefit in a High-Speed Axial Compressor
GT 1997; V001T03A110https://doi.org/10.1115/97-GT-535
Topics:
Compressors
,
Wakes
,
Rotors
,
Stators
,
Energy dissipation
,
Lasers
,
Simulation
,
Design
,
Flow (Dynamics)
,
Fluids
Microturbines and Small Turbomachinery
Research and Development of 300kW Class Ceramic Gas Turbine Project in Japan
GT 1997; V001T04A001https://doi.org/10.1115/97-GT-087
Topics:
Ceramics
,
Gas turbines
,
Industrial research
,
Thermal efficiency
,
Blades
,
Engines
,
Combustion chambers
,
Emissions
,
Engineering prototypes
,
Nitrogen oxides
Progress on the Hybrid Vehicle Turbine Engine Technology Support (HVTE-TS) Program
GT 1997; V001T04A002https://doi.org/10.1115/97-GT-088
Topics:
Gas turbines
,
Hybrid electric vehicles
,
Industrial ceramics
,
Insulation
,
Testing
,
Automotive industry
,
Ceramics
,
Combustion systems
,
Design
,
Durability
Development in the Full Assembly Test Rig of the 100kW Automotive Ceramic Gas Turbine
GT 1997; V001T04A004https://doi.org/10.1115/97-GT-210
Topics:
Automotive gas turbines
,
Manufacturing
,
Automobiles
,
Emissions
,
Gasoline
,
Natural resources
,
Petroleum
,
Regulations
,
Temperature
,
Thermal efficiency
Thermo-Economics of a Small 50 KW Turbogenerator
GT 1997; V001T04A005https://doi.org/10.1115/97-GT-260
Topics:
Thermoeconomics
,
Turbogenerators
,
Engines
,
Ceramics
,
Gas turbines
,
Thermal efficiency
,
Design
,
Manufacturing
,
Rotors
,
Brayton cycle
Foil Air/Gas Bearing Technology — An Overview
GT 1997; V001T04A006https://doi.org/10.1115/97-GT-347
Topics:
Air bearings
,
Aircraft
,
Analytical methods
,
Cycles
,
Failure
,
Fluids
,
Foil bearings
,
Gas bearings
,
Gases
,
High temperature
Economics and Design Approaches for Small Commercial Turbogenerators
GT 1997; V001T04A007https://doi.org/10.1115/97-GT-364
Topics:
Design
,
Economics
,
Turbogenerators
,
Aerospace industry
,
Manufacturing
,
Innovation
Current Status of CGT302 (Progressing to Final Phase)
GT 1997; V001T04A009https://doi.org/10.1115/97-GT-461
Topics:
Airfoils
,
Blades
,
Ceramics
,
Combustion chambers
,
Compressors
,
Damage
,
Durability
,
Emissions
,
Engines
,
Gas turbines
Ceramic Heat Exchangers-The Key to High Efficiency in Very Small Gas Turbines
GT 1997; V001T04A011https://doi.org/10.1115/97-GT-463
Topics:
Ceramics
,
Gas turbines
,
Heat
,
Engines
,
Heat exchangers
,
Maintenance
,
Reliability
,
Turbines
,
Compressors
,
Cycles
Facilities for Automotive Gas Turbine Ceramic Components
GT 1997; V001T04A012https://doi.org/10.1115/97-GT-464
Topics:
Automotive gas turbines
,
Brakes
,
Ceramics
,
Combustion chambers
,
Compressors
,
Data acquisition
,
Ducts
,
Heat exchangers
,
Industrial ceramics
,
Particle spin
Ceramic Gas Turbine Technology Development
GT 1997; V001T04A013https://doi.org/10.1115/97-GT-465
Topics:
Ceramics
,
Gas turbines
,
Technology development
,
Engines
,
Industrial ceramics
,
Turbine blades
,
Testing
,
Manufacturing
,
Experimental design
,
NASA