SAWE Technical Papers

Showing 1921–1936 of 2059 results

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  82. Structural Weight Estimation for the Initial Stage of Preliminary Design

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  822. Weight Optimization Using Geometric Programming

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  823. Parameter Alteration in a Computer-Aided Mechanical Engineering Design System

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  824. Weight Analysis Automation Using Remote Terminal Deskside Time-Shared Computer System

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  826. Minimum Weight Analysis of Fuselage Frames

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  827. Aerospace Weight Savings Through Advanced Abrasive Machining

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  828. Shape Factors for Structural Weight Prediction and Optimization

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  829. An Analytical Approach to Landing Gear Weight Estimation

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  83. Simulation of Airplane Mass Properties in the Design and Construction of Wind Tunnel Flutter Models

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  835. Loadability of ‘Concorde’

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  836. A Computerized Approach to Aircraft Loadability

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  837. Lockheed L-1011 On-Board Weight and Balance System

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  838. A Definition of the Aircraft Stretch Efficiency Factor

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  839. A Theoretical Contribution to the Study of Weight Growth Factor in Aircraft Design

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  84. Consideration of Bending and Torsional Stiffness in the Design of Wings for Minimum Weight

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  840. Balancing Options in Aircraft Configuration Design

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