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SAWE0081 |
81. A Weight Control Procedure for Gas Turbine Engines |
$20.00 |
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SAWE0810 |
810. The Derivation and Application of Analytical-Statistical Weight Prediction Techniques |
$20.00 |
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|
SAWE0811 |
811. An Automated System for Mass Properties Data Control |
$20.00 |
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|
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 |
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|
SAWE0814 |
814. Structural Optimization - A Dream or a Reality? |
$20.00 |
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|
SAWE0816 |
816. Considerations in the Calibration on Electronic Load Cells |
$20.00 |
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|
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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