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Instrumentation for airbreathing propulsion : technical papers selected from the Symposium on Instrumentation for Airbreathing Propulsion, September 1972, subsequently revised for this volume /
| Clasificación: | Libro Electrónico |
|---|---|
| Autores Corporativos: | , |
| Otros Autores: | , |
| Formato: | Electrónico Congresos, conferencias eBook |
| Idioma: | Inglés |
| Publicado: |
Cambridge, Mass. :
MIT Press,
1974.
|
| Colección: | Progress in astronautics and aeronautics ;
v. 34. |
| Temas: | |
| Acceso en línea: | Texto completo |
Tabla de Contenidos:
- Cover
- Title
- Copyright
- Contents
- Preface
- Symposium Committees
- I Inlet Internal Flow
- Response of Miniature Pressure Transducers to Fluctuations in Supersonic Flow
- Research Instrumentation Requirements for Flight/Wind-Tunnel Tests of the YF-12 Propulsion System and Related Flight Experience
- Instrumentation for In-Flight Determination of Steady-State and Dynamic Inlet Performance in Supersonic Aircraft
- System for Evaluation of F-15 Inlet Dynamic Distortion
- Application of Laser Velocimeters for Flow Measurements
- Investigation of the Use of Holography in Studying Supersonic Flow in InletsII Compressor Internal Aerodynamics
- On the Determination of the Internal Aerodynamics of Compressors
- Dynamic Flow Studies by Application of Pressure and Velocity Sensors on Axial Flow Fan Blades
- On-the-Shaft Data Systems for Rotating Engine Components
- Laser Velocimeter System Development and Testing
- Effect of Transducer Diameter on Resolution of Total Pressure Fluctuations in a Turbulent Flow
- Measurement of Instantaneous Air Angle and Total Temperature Fluctuations behind Transonic Compressor RotorsTotal Pressure Averaging in Pulsating Flows
- Modularized Instrument System for Turbojet Engine Test Facilities
- Fiber Optic and Laser Digital Pressure Transducers
- III Turbojet, Ramjet, and Composite Combustors
- Current State-of-the-Art for Airbreathing Combustor Measurements
- Holography of Nozzles, Jets, and Spraying Systems
- Measurement Techniques for Supersonic Combustion Testing
- Application of Raman Effect to Flowfield Diagnostics
- Holography of JP-4 Droplets and Combusting Boron ParticlesIV Turbines
- Use of Laser-Powered Optical Proximity Probe in Advanced Turbofan Engine Development
- Study of a Flight Monitor for Jet Engine Disk Cracks Using the Critical Length Criterion of Fracture Mechanics
- Heat Transfer Measurements in Turbines
- Pyrometer for Measurement of Surface Temperature Distribution on a Rotating Turbine Blade
- Gas Temperature-Density (GTD) Sensor for Turbine Inlet Gas Temperature Measurement
- Advances in Measuring Techniques for Turbine Cooling Test Rigs: Status Report
- Instrumenting a Stoichiometric Turbine Development EngineV Propulsion Controls
- Turbine Blade Pyrometer System in the Control of the Concorde Engine
- Experiences in the Design and Application of Turbine Blade Pyrometers
- Engine Sensory Requirements for Energy Management
- An Ultrasonic Turbine Inlet Gas Temperature Sensor
- Automatic Detection and Suppression of Inlet Buzz
- VI Engine Condition Monitoring
- Engine Condition Monitoring as a Part of the Propulsion Management Concept
- Inflight Engine Condition Monitoring System