Forum 65 - Grapevine, TX 2009
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Preliminary Axial Flow Turbine Design and Off-Design Analysis Methods for Rotary Wing Aircraft Engines; I - Validation Regular Price: $30.00 Member price: $15.00
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Preliminary Axial Flow Turbine Design and Off-Design Analysis Methods for Rotary Wing Aircraft Engines; II - Applications Regular Price: $30.00 Member price: $15.00
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Compressor Study to Meet Large Civil Tilt Rotor Engine Requirements Regular Price: $30.00 Member price: $15.00
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H-60 Tail Rotor Drive Shaft Thomas Coupling Transient Overload Capacity Regular Price: $30.00 Member price: $15.00
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Load Sharing Test of the CH-53K Split Torque Main Gearbox Regular Price: $30.00 Member price: $15.00
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Measurements of Drag Torque, Lift-Off Journal Speed and Temperature in a Metal Mesh Foil Bearing Regular Price: $30.00 Member price: $15.00
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Gas Turbine Characteristics for a Large Civil Tilt-Rotor (LCTR) Regular Price: $30.00 Member price: $15.00
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Double Helical Gear Performance Results in High Speed Helical Gear Trains Regular Price: $30.00 Member price: $15.00
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Rotary-Wing Relevant Compressor Aero Research and Technology Development Activities at Glenn Research Center Regular Price: $30.00 Member price: $15.00
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RDS-21 Demonstrator Gearbox Testing Regular Price: $30.00 Member price: $15.00
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Advanced Adaptive Model-Based Engine Control, Engine Test Results Regular Price: $30.00 Member price: $15.00
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Face Gear Development Under the Rotorcraft Drive System for the 21st Century Program Regular Price: $30.00 Member price: $15.00
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Foil Bearing Starting Considerations and Requirements for Rotorcraft Engine Applications Regular Price: $30.00 Member price: $15.00
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Advancements Toward Oil-Free Rotorcraft Propulsion Regular Price: $30.00 Member price: $15.00
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Lichten Award Winning Paper: CFD Investigation of Engine Exhaust Swirling Flow in High Aspect Ratio Rectangular Ducts Regular Price: $30.00 Member price: $15.00
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Thermohydrodynamic Model Predictions and Performance Measurements of Bump-Type Foil Bearing for Oil-Free Turboshaft Engines in Rotorcraft Propulsion Systems Regular Price: $30.00 Member price: $15.00
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The Case for Distributed Engine Control in Turbo-Shaft Engine Systems Regular Price: $30.00 Member price: $15.00
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Establishing a Ballistic Test Methodology for Documenting the Containment Capability of Small Gas Turbine Engine Compressors Regular Price: $30.00 Member price: $15.00
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CFD Investigation Of Engine Exhaust Swirling Flow In High Aspect Ratio Rectangular Ducts Regular Price: $30.00 Member price: $15.00
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Test and Evaluation of Foil Air Bearings for use in an Advanced Turboshaft Engine Regular Price: $30.00 Member price: $15.00
