Technical Papers

SKU Title Price
SAWE0081 81. A Weight Control Procedure for Gas Turbine Engines $20.00
SAWE0810 810. The Derivation and Application of Analytical-Statistical Weight Prediction Techniques $20.00
SAWE0811 811. An Automated System for Mass Properties Data Control $20.00
SAWE0812 812. A Parametric Approach to Estimating Weights of Surface Control Systems of Combat and Transport Aircraft $20.00
SAWE0813 813. On the Use of Aircraft Density in Preliminary Design $20.00
SAWE0814 814. Structural Optimization - A Dream or a Reality? $20.00
SAWE0816 816. Considerations in the Calibration on Electronic Load Cells $20.00
SAWE0817 817. Angle of Inclination From One Measuring System $20.00
SAWE0818 818. Aerodynamics Effects on the Measurement of Mass Properties Using a Trebel Dynamic Balancing Machine $20.00
SAWE0082 82. Structural Weight Estimation for the Initial Stage of Preliminary Design $24.00
SAWE0822 822. Weight Optimization Using Geometric Programming $20.00
SAWE0823 823. Parameter Alteration in a Computer-Aided Mechanical Engineering Design System $20.00
SAWE0824 824. Weight Analysis Automation Using Remote Terminal Deskside Time-Shared Computer System $20.00
SAWE0826 826. Minimum Weight Analysis of Fuselage Frames $26.50
SAWE0827 827. Aerospace Weight Savings Through Advanced Abrasive Machining $20.00
SAWE0828 828. Shape Factors for Structural Weight Prediction and Optimization $20.00
SAWE0829 829. An Analytical Approach to Landing Gear Weight Estimation $20.00
SAWE0083 83. Simulation of Airplane Mass Properties in the Design and Construction of Wind Tunnel Flutter Models $20.00
SAWE0835 835. Loadability of 'Concorde' $20.00
SAWE0836 836. A Computerized Approach to Aircraft Loadability $20.00
SAWE0837 837. Lockheed L-1011 On-Board Weight and Balance System $20.00
SAWE0838 838. A Definition of the Aircraft Stretch Efficiency Factor $20.00
SAWE0839 839. A Theoretical Contribution to the Study of Weight Growth Factor in Aircraft Design $20.00
SAWE0084 84. Consideration of Bending and Torsional Stiffness in the Design of Wings for Minimum Weight $20.00
SAWE0840 840. Balancing Options in Aircraft Configuration Design $20.50

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