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Hamilton Standard Div., United Aircraft Corp.
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Effect of Inlet Normal Shock Position Control Systems on Range of Supersonic Transports

Published 1961-01-01 by SAE International in United States
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High-Voltage Electron Beam Welding of Aerospace Components

Published 1962-01-01 by SAE International in United States
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Development of a Lumped Parameter Model for a Monopropellant Hydrazine Reaction Chamber

Published 1967-02-01 by SAE International in United States
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Propeller Design Consideration for Turbine Powered Aircraft

Published 1968-02-01 by SAE International in United States
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Programmed Testing Systems - Turbine Engines and Accessories

Published 1968-02-01 by SAE International in United States
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High Altitude/Cold Weather Operation of Hamilton Standard Propellers

Published 1969-02-01 by SAE International in United States
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Engine Air Inlet Compatibility for the Supersonic Transport

Published 1965-02-01 by SAE International in United States
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Propulsion Control Integration for Power Management

Published 1970-02-01 by SAE International in United States
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New Low-Pressure-Ratio Fans for Quiet Business Aircraft Propulsion

Published 1973-02-01 by SAE International in United States
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Methods to Achieve Nationwide Automotive Diagnostic Testing

Published 1973-02-01 by SAE International in United States
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