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Proceedings Papers
In This Volume
Volume 1A: General
General
Rotor Burst Protection Program: Statistics on Aircraft Gas Turbine Engine Rotor Failures That Occurred in U. S. Commercial Aviation During 1973
GT 1975; V01AT01A011https://doi.org/10.1115/75-GT-12
Topics:
Aircraft
,
Commercial air transport
,
Failure
,
Gas turbines
,
Rotors
,
Statistics
,
Engines
,
Aviation
,
Flight
A Study on the Flow Mechanism Within Centrifugal Impeller Channels
GT 1975; V01AT01A013https://doi.org/10.1115/75-GT-14
Topics:
Flow (Dynamics)
,
Impellers
,
Design
,
Blades
,
Diffusion (Physics)
,
Probes
,
Reliability
,
Yaw
Heat Transfer Analysis Along the Blades of a Gas Turbine Stator by Thermal and Kinematic Boundary Layers Theory
GT 1975; V01AT01A014https://doi.org/10.1115/75-GT-15
Topics:
Blades
,
Boundary layers
,
Gas turbines
,
Heat transfer
,
Kinematics
,
Stators
,
Turbulence
,
Boundary-value problems
,
Compressible flow
,
Flow (Dynamics)
A Technical and Economic Overview of the Benefits of Repowering
GT 1975; V01AT01A015https://doi.org/10.1115/75-GT-16
Topics:
Boilers
,
Combustion
,
Heat recovery
,
Steam turbines
,
Thermal power stations
,
Turbines
Attenuation of Acoustic Energy Across a Turbine Stage With Subsonic Relative Flow
GT 1975; V01AT01A016https://doi.org/10.1115/75-GT-17
Topics:
Acoustics
,
Flow (Dynamics)
,
Turbines
,
Actuators
,
Disks
,
Flow turning
,
Mach number
Industrial Gas Turbine Materials and Some Service Experiences
GT 1975; V01AT01A018https://doi.org/10.1115/75-GT-19
Topics:
Industrial gases
,
Turbines
,
Construction
,
Design
,
Fuels
,
Gas turbines
,
Lubricating oils
,
Temperature
The Vorbix Burner: A New Approach to Gas Turbine Combustors
GT 1975; V01AT01A019https://doi.org/10.1115/75-GT-20
Topics:
Combustion chambers
,
Gas turbines
,
Combustion
,
Fuels
,
Design
,
Emissions
,
Fuel systems
,
Performance characterization
,
Stability
,
Swirling flow
The Refracting Inlet: A New Concept for Aircraft Inlet Noise Suppression
GT 1975; V01AT01A020https://doi.org/10.1115/75-GT-21
Topics:
Aircraft
,
Noise (Sound)
,
Refraction
,
Gas turbines
,
Waves
The Mach 2 Axial Flow Compressor Stage
GT 1975; V01AT01A021https://doi.org/10.1115/75-GT-22
Topics:
Axial flow
,
Compressors
,
Geometry
,
High pressure (Physics)
,
Inlet guide vanes
,
Mach number
,
Rotors
Investigation of the Axial Velocity Density Ratio in a High Turning Cascade
GT 1975; V01AT01A024https://doi.org/10.1115/75-GT-25
Topics:
Cascades (Fluid dynamics)
,
Density
,
Turning
,
Blades
,
Flow (Dynamics)
,
Stators
,
Mach number
The Supersonic Axial Inlet Component in a Compressor
GT 1975; V01AT01A025https://doi.org/10.1115/75-GT-26
Topics:
Compressors
,
Mach number
,
Nozzles
,
Blades
,
Design
,
Ducts
,
Dynamic response
,
Engineering prototypes
,
Failure
,
Rotors
Recuperator Development Trends for Future High Temperature Gas Turbines
GT 1975; V01AT01A049https://doi.org/10.1115/75-GT-50
Topics:
Gas turbines
,
High temperature
,
Ceramics
,
Cycles
,
Heat exchangers
,
Combustion chambers
,
Design
,
Ducts
,
Emissions
,
Engines
Review of a Combined Steam and Gas Turbine Cycle for Pipeline Service
GT 1975; V01AT01A050https://doi.org/10.1115/75-GT-51
Topics:
Cycles
,
Gas turbines
,
Pipelines
,
Steam
,
Combined cycles
,
Climate
,
Fuels
,
Stress
,
Temperature
,
Turbines
Isothermal Shape Rolling of Airfoil Sections for Gas Turbines
GT 1975; V01AT01A051https://doi.org/10.1115/75-GT-52
Topics:
Airfoils
,
Gas turbines
,
Shapes
,
Contamination
,
Corrosion
,
Electric current
,
Finishes
,
Heating
,
Metals
,
Refractory metals
Early Experience With a 31,050-Hp Regenerative Cycle Gas Turbine
GT 1975; V01AT01A052https://doi.org/10.1115/75-GT-53
Topics:
Cycles
,
Gas turbines
,
Compressors
,
Economics
,
Fuels
,
Natural gas
,
Pipelines
,
Turbines
Graphic Design and Numerical Control Programming for Turbo-Rotor Manufacturing
GT 1975; V01AT01A055https://doi.org/10.1115/75-GT-56
Topics:
Computer programming
,
Design
,
Manufacturing
,
Rotors
,
Turbochargers
,
Machinery
,
Computers
,
Milling
,
Turbomachinery
Transient Response Analysis of Damped Rotor Systems by the Normal Mode Method
GT 1975; V01AT01A057https://doi.org/10.1115/75-GT-58
Topics:
Rotors
,
Transients (Dynamics)
,
Springs
,
Eigenvalues
,
Steady state
,
Stress
,
Transient analysis
,
Dampers
,
Damping
,
Displacement
Propagating Stall in Compressors With Porous Walls
GT 1975; V01AT01A058https://doi.org/10.1115/75-GT-59
Topics:
Compressors
,
Blades
,
Cascades (Fluid dynamics)
,
Delays
,
Flow (Dynamics)
,
Flow instability
,
Radial flow
,
Unsteady flow
A Study of Casing Treatment Stall Margin Improvement Phenomena
GT 1975; V01AT01A059https://doi.org/10.1115/75-GT-60
Topics:
Annulus
,
Blades
,
Boundary layers
,
Chords (Trusses)
,
Compressors
,
Diluents
,
Flow (Dynamics)
,
Pressure
,
Pressure gradient
,
Rotors
Excess Noise From Gas Turbine Exhausts
GT 1975; V01AT01A060https://doi.org/10.1115/75-GT-61
Topics:
Gas turbines
,
Noise (Sound)
,
Acoustics
,
Temperature
,
Turbines
,
Blades
,
Combustion chambers
,
Engines
,
Exhaust systems
,
Flow (Dynamics)
Cascade Research on a Small, Axial, High-Work, Cooled Turbine
GT 1975; V01AT01A061https://doi.org/10.1115/75-GT-62
Topics:
Cascades (Fluid dynamics)
,
Turbines
,
Flow (Dynamics)
,
Design
,
Engines
,
Nozzles
,
Rotors
,
Blades
,
Cooling
,
Degrees of freedom