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× 3237. Obtaining Optimal Results with Filar Pendulums for Moment of Inertia Measurements 3237. Obtaining Optimal Results with Filar Pendulums for Moment of Inertia Measurements $20.00
$20.00
× 3116. Utilizing High Thermal Conductivity Graphite Foam to Improve Heat Exchanger Performance 3116. Utilizing High Thermal Conductivity Graphite Foam to Improve Heat Exchanger Performance $20.00
$20.00
× 3131. Weight Focused Workshops - Overcoming Inhibitors to Implementation 3131. Weight Focused Workshops - Overcoming Inhibitors to Implementation $20.00
$20.00
× 3172. Advanced Tiltrotor Design 3172. Advanced Tiltrotor Design $20.00
$20.00
× 3117. The Development of Sea Launch Mass Properties 3117. The Development of Sea Launch Mass Properties $20.00
$20.00
× 3233. Fuel Analysis: Methods, Techniques, and Calibration 3233. Fuel Analysis: Methods, Techniques, and Calibration $20.00
$20.00
× 3232. Vendetta: Supercruising Future Strike Aircraft On CD-R 3232. Vendetta: Supercruising Future Strike Aircraft On CD-R $20.00
$20.00
× 3126. The General Aviation Revitalization Act Causes and Consequences 3126. The General Aviation Revitalization Act Causes and Consequences $20.00
$20.00
× 3129. Ford's Weight Engineering Academy 3129. Ford's Weight Engineering Academy $20.00
$20.00
× 3141. Frame Design Parameters and Techniques Applied In SAE's Collegiate Mini Baja Competition 3141. Frame Design Parameters and Techniques Applied In SAE's Collegiate Mini Baja Competition $20.00
$20.00
× 3130. Inertia Measurements of Large MilitaryVehicles 3130. Inertia Measurements of Large MilitaryVehicles $20.00
$20.00
× 3111. A Proven Waterborne Coating 3111. A Proven Waterborne Coating $20.00
$20.00
× 3113. Composite Ejector Door Design Concept Evaluation for the HSCT Engine Nozzle 3113. Composite Ejector Door Design Concept Evaluation for the HSCT Engine Nozzle $20.00
$20.00
× 23. The Value of a Pound 23. The Value of a Pound $20.00
$20.00
× 30. The Effect of Center of Gravity on Performance 30. The Effect of Center of Gravity on Performance $20.00
$20.00
× 22. Preliminary Design Equations for Aircraft Weight Estimation 22. Preliminary Design Equations for Aircraft Weight Estimation $20.00
$20.00
× 32. Weight and It's Effect on the Operation and Performance of Commercial Aircraft 32. Weight and It's Effect on the Operation and Performance of Commercial Aircraft $20.00
$20.00

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Subtotal $340.00
Tax $0.00
Total $340.00