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For Corporate Partners and Company Members with an active membership, documents associated with membership benefits are made accessible on SAWE cloud services.  The copying/distribution restrictions highlighted above still apply. Please contact the SAWE Executive Director for questions or concerns.

Remove item Thumbnail image Product Price Quantity Subtotal
× 30. The Effect of Center of Gravity on Performance 30. The Effect of Center of Gravity on Performance $20.00
$20.00
× 34. Pneumatic Controls for Aircraft 34. Pneumatic Controls for Aircraft $20.00
$20.00
× 7. Predetermination of Weight Efficiency 7. Predetermination of Weight Efficiency $20.00
$20.00
× 3. Aircraft Accessories - A Weighty Problem 3. Aircraft Accessories - A Weighty Problem $20.00
$20.00
× 8. A Practical Method for Wing Weight Estimation 8. A Practical Method for Wing Weight Estimation $20.00
$20.00
× 14. Weight Predictor 14. Weight Predictor $20.00
$20.00
× 35. A Graphical Method of Preparing Tabular Schedules for Balance Control in Loading Passenger Transport Aircraft 35. A Graphical Method of Preparing Tabular Schedules for Balance Control in Loading Passenger Transport Aircraft $20.00
$20.00
× 22. Preliminary Design Equations for Aircraft Weight Estimation 22. Preliminary Design Equations for Aircraft Weight Estimation $20.00
$20.00
× 33. Some Problems in the Selection of Optimum Airplane Configurations for Minimum Weight 33. Some Problems in the Selection of Optimum Airplane Configurations for Minimum Weight $20.00
$20.00
× 10. Calculation of Landing Gear and Hydraulic System Weights 10. Calculation of Landing Gear and Hydraulic System Weights $20.00
$20.00
× 1070. The Integrated Team: Key to Implementing Design-To-Cost 1070. The Integrated Team: Key to Implementing Design-To-Cost $20.00
$20.00
× 1095. USAF In-Service Weight and Balance System 1095. USAF In-Service Weight and Balance System $20.00
$20.00
× 1056. The Challenge of Weight and Balance Control and Design-To-Cost for Y/C-14 Prototype Development 1056. The Challenge of Weight and Balance Control and Design-To-Cost for Y/C-14 Prototype Development $20.00
$20.00
× 1068. Will Design-To-Cost Work Over the Long Haul? 1068. Will Design-To-Cost Work Over the Long Haul? $20.00
$20.00
× 1094. A Loadability Comparison of the L-1011 and DC-10-10 1094. A Loadability Comparison of the L-1011 and DC-10-10 $20.00
$20.00
× 1063. Isogrid Weight Optimum Structures 1063. Isogrid Weight Optimum Structures $20.00
$20.00
× 1071. A Parametric Determination of Transport Aircraft Price 1071. A Parametric Determination of Transport Aircraft Price $20.00
$20.00
× 20. Wing Weight Estimating Simplified 20. Wing Weight Estimating Simplified $20.00
$20.00
× 1104. Weight and Balance Considerations in the Design of the A-10A Close Air Support Aircraft 1104. Weight and Balance Considerations in the Design of the A-10A Close Air Support Aircraft $20.00
$20.00
× 1091. Weight Contribution to Fuel Conservation for Terminal Area Compatible Aircraft 1091. Weight Contribution to Fuel Conservation for Terminal Area Compatible Aircraft $20.00
$20.00
× 1843. Center of Gravity Control on Airbus Aircraft: Fuel Range and Loading Benefits 1843. Center of Gravity Control on Airbus Aircraft: Fuel Range and Loading Benefits $20.00
$20.00
× 1829. A Low Speed Dyunamic Balance System 1829. A Low Speed Dyunamic Balance System $20.00
$20.00
× 1840. Lodability Consideration in Preliminary Design 1840. Lodability Consideration in Preliminary Design $20.00
$20.00
× 1835. Integrating Cadam, Timesharing Option, the Personal Computer, and the Word Processing for Mass Properties Calculation and 1835. Integrating Cadam, Timesharing Option, the Personal Computer, and the Word Processing for Mass Properties Calculation and $20.00
$20.00

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Cart totals

Subtotal $480.00
Tax $0.00
Total $480.00
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