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Analysis of Transients in Gas-Propulsion Systems with Attitude Control Rocket System
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F. Martelli,
Published/Copyright:
December 1, 1993
Published Online: 1993-12
©2011 by Walter de Gruyter GmbH & Co.
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Articles in the same Issue
- CONTENTS
- Oscillating Aerodynamics and Flutter of an Aerodynamically Detuned Cascade in an Incompressible Flow
- A Unified Variable-Domain Variational Approach to Hybrid Problems of Compressible Blade-to-Blade Flow
- The Effect of High Reduced Frequency Values on Compressor Blade Row Gust Response
- Analysis of Transients in Gas-Propulsion Systems with Attitude Control Rocket System
- A Theoretical Study of Polydisperse Spray Diffusion Flames in the Far Field of a Fuel-Injector
- Coalescence Effects in Vaporizing Polydisperse Fuel-Sprays Suspended in a 3-D Axisymmetric Stagnation Flow
Articles in the same Issue
- CONTENTS
- Oscillating Aerodynamics and Flutter of an Aerodynamically Detuned Cascade in an Incompressible Flow
- A Unified Variable-Domain Variational Approach to Hybrid Problems of Compressible Blade-to-Blade Flow
- The Effect of High Reduced Frequency Values on Compressor Blade Row Gust Response
- Analysis of Transients in Gas-Propulsion Systems with Attitude Control Rocket System
- A Theoretical Study of Polydisperse Spray Diffusion Flames in the Far Field of a Fuel-Injector
- Coalescence Effects in Vaporizing Polydisperse Fuel-Sprays Suspended in a 3-D Axisymmetric Stagnation Flow
