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All SAWE books, technical papers, recommended practices, and handbooks which are published/distributed by SAWE are SAWE copyrighted property. Anyone who does any of the following without authorization from SAWE infringes on that copyright:

  • Reproduce the work by making copies of it
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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
× 1854. The Importance of Weight in Changing a Cost Estimating Environment 1854. The Importance of Weight in Changing a Cost Estimating Environment $20.00
$20.00
× 1848. Beryllium Application and Engineering 1848. Beryllium Application and Engineering $20.00
$20.00

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Subtotal $440.00
Tax $0.00
Total $440.00
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