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Thrust Vectoring Flight Control To Maximize Future Jet Transport Flight Safety
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Benjamin Gal-Or,
Veröffentlicht/Copyright:
1. März 2001
Published Online: 2001-03
©2011 by Walter de Gruyter GmbH & Co.
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Artikel in diesem Heft
- CONTENTS
- The Effects of Blade Count on Boundary Layer Development in a Low-Pressure Turbine
- Effects of Hot Streak Shape on Rotor Heating in a High-Subsonic Single-Stage Turbine
- A Simple Method for Geometry Definition of Radial Compressors
- Advanced Aerothermodynamics Associated with Clean Technologies for Upgrading Gas Turbines in Simple and Combined-Cycle Power Stations
- Thrust Vectoring Flight Control To Maximize Future Jet Transport Flight Safety
- Simultaneous Prediction of External Flow-Field and Temperature in Internally Cooled 3-D Turbine Blade Material
- A Simple Mobile Anechoic Chamber For Experiments in Jet Acoustics
- The Influence of Fuel Droplet Characteristics on Chemical Mechanisms in a Premixed Laminar Spray Flame
Artikel in diesem Heft
- CONTENTS
- The Effects of Blade Count on Boundary Layer Development in a Low-Pressure Turbine
- Effects of Hot Streak Shape on Rotor Heating in a High-Subsonic Single-Stage Turbine
- A Simple Method for Geometry Definition of Radial Compressors
- Advanced Aerothermodynamics Associated with Clean Technologies for Upgrading Gas Turbines in Simple and Combined-Cycle Power Stations
- Thrust Vectoring Flight Control To Maximize Future Jet Transport Flight Safety
- Simultaneous Prediction of External Flow-Field and Temperature in Internally Cooled 3-D Turbine Blade Material
- A Simple Mobile Anechoic Chamber For Experiments in Jet Acoustics
- The Influence of Fuel Droplet Characteristics on Chemical Mechanisms in a Premixed Laminar Spray Flame
