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An Assessment of Supersonic Gas Turbine Missile Propulsion Potential
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Eli H. Benstein,
Published/Copyright:
June 1, 1991
Published Online: 1991-06
©2011 by Walter de Gruyter GmbH & Co.
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Articles in the same Issue
- CONTENTS
- Three Dimensional Cascade Aerodynamics Including Non-Uniform Inlet Flow Effects
- Feasibility Study of Using Bleeded Air from a Turbocharger System for Air-Conditioning Purposes
- Distributions of Velocities and Void Fractions in a Radial-Flow Pump Impeller Handling Air- Water Two-Phase Mixtures
- Linear Modeling of a Marine Gas Turbine Propulsion Plant
- The Microflows Within the Tip Clearance Gap of an Unshrouded Axial Turbine and Their Effects on Loss Development
- Thermal and Mechanical Properties of Thermal Barrier Coatings
- 3-D Axial Blade Row Flow Field Inviscid Finite Volume Prediction and Verification
- An Assessment of Supersonic Gas Turbine Missile Propulsion Potential
- Computation of Turbulent Flow Through Strongly Curved Ducts and End-Wall Flows in Cascades Using a Space-Marching Method
- The Unsteady State Simulation of Gas Turbine Engines for Training Purposes
Articles in the same Issue
- CONTENTS
- Three Dimensional Cascade Aerodynamics Including Non-Uniform Inlet Flow Effects
- Feasibility Study of Using Bleeded Air from a Turbocharger System for Air-Conditioning Purposes
- Distributions of Velocities and Void Fractions in a Radial-Flow Pump Impeller Handling Air- Water Two-Phase Mixtures
- Linear Modeling of a Marine Gas Turbine Propulsion Plant
- The Microflows Within the Tip Clearance Gap of an Unshrouded Axial Turbine and Their Effects on Loss Development
- Thermal and Mechanical Properties of Thermal Barrier Coatings
- 3-D Axial Blade Row Flow Field Inviscid Finite Volume Prediction and Verification
- An Assessment of Supersonic Gas Turbine Missile Propulsion Potential
- Computation of Turbulent Flow Through Strongly Curved Ducts and End-Wall Flows in Cascades Using a Space-Marching Method
- The Unsteady State Simulation of Gas Turbine Engines for Training Purposes