Computational Design of Turbomachine Blades

Volume 17, Number 5May 1980

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Topics

• Aerodynamics
• Aerospace Sciences
• Air Intake Design
• Airbreathing Jet Engine
• Aircraft Design
• Aircraft Engine Design
• Aircraft Engines
• Aircraft Operations and Technology
• Compressors
• Flow Regimes
• Fluid Dynamics
• Jet Engines
• Marine Propulsion
• Propulsion and Power
• Subsonic Inlets
• Supersonic Inlets
• Turbomachinery

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Keywords

• Turbomachine Blades
• Mach Numbers
• Computer Programs
• Axial Flow Compressor
• Supersonic Flow
• Mass Flow
• Aerothermodynamic Relations
• Flow Distribution
• Continuity Equation
• Iterative Solution

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Digital

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• Published online22 May 2012