What's New!
Aviation Maintenance Technician Handbook–Powerplant (FAA-H-8083-32A) Volume 2
Aviation Maintenance Technician Handbook–Powerplant (FAA-H-8083-32A) Volume 2 is designed to aid students enrolled in a formal course of instruction, as well as the individual who is studying on his or her own. Since the knowledge requirements for the airframe and powerplant ratings closely parallel each other in some subject areas, the chapters which discuss fire protection systems and electrical systems contain some material which is also duplicated in the Aviation Maintenance Technician Handbook–Airframe (FAA-H-8083-31A). |
Aviation Maintenance Technician Handbook–Powerplant Volume 1
The Aviation Maintenance Technician Handbook–Powerplant (FAA-H-8083-32A) is one of a series of three handbooks for persons preparing for certification as a powerplant mechanic. It is intended that this handbook provide the basic information on principles, fundamentals, and technical procedures in the subject matter areas relating to the powerplant rating. |
C-Section No. 2 of 1b Loading Concentrated Intermediate Torque applied Deflection and Stress Equatio
C-Section with Concentrated Intermediate Torque applied Deflection and Stress Equations and Calculator #2 of 1b Loading .
Loading configuration left end free to twist and warp right end fixed (no twist or warp). Formulas for the elastic deformations of uniform thin-walled open members under torsional loading.
Per. Roarks Formulas for Stress and Strain - Formulas for torsional properties and stresses in thin-walled open cross sections, Table 10.2. |
Double Y Section with Concentrated Intermediate Torsional Loading Per. Roarks Formulas
Double Y Section with Concentrated Intermediate Torsional Loading Applied Deflection and Stress Equations and Calculator #11 of 1a Loading. Formulas for the elastic deformations of uniform thin-walled open members under torsional loading. Per. Roarks Formulas for Stress and Strain - Formulas for torsional properties and stresses in thin-walled open cross sections, Table 10.2, Row 11. |
Z-Section Flange Beam Intermediate Torsional Loading Equations and Calculator
Z-Section Flange Beam with Concentrated Intermediate Torsional Loading Applied Deflection and Stress Equations and Calculator #8 of 1a Loading. Formulas for the elastic deformations of uniform thin-walled open members under torsional loading. Per. Roarks Formulas for Stress and Strain - Formulas for torsional properties and stresses in thin-walled open cross sections, Table 10.2. |
Channel Section with Left End Free to Twist Right End Fixed Equations and Calculator
Channel Section with Left end free to twist and warp right end fixed (no twist or warp) Deflection and Stress Equations and Calculator.
Formulas for the elastic deformations of uniform thin-walled open members under torsional loading. Per. Roarks Formulas for Stress and Strain Formulas for torsional properties and stresses in thin-walled open cross sections, Table 10.2, Loading Configuration 1b. |
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What's New!
Solar Sail Design and Fabrication Assessment
Spinning Sail Blade, Square Sail Blade study and evaluation of designs and fabrication methods, equipment, facilities, economics, schedules, etc., for the square sail sheet alternate. Those efforts and the work accomplished, until redirected to focus attention on the spinning sail blade alternate, are documented in Section II of this report. |
Twin Channel With Flanges Outward Intermediate Torsional Applied No 5 Per. Roarks Formulas
Twin Channel With Flanges Outward Section with Concentrated Intermediate Torque applied Deflection and Stress Equations and Calculator #5 of 1a Loading. Formulas for the elastic deformations of uniform thin-walled open members under torsional loading. Per. Roarks Formulas for Stress and Strain - Formulas for torsional properties and stresses in thin-walled open cross sections, Table 10.2. |
Circular Ring Analysis No 21 Roarks Formulas for Stress and Strain Equations and Calculator
Circular Ring Moment, Hoop Load, and Radial Shear Equations and Calculator Per. Roarks Formulas for Stress and Strain Formulas for Circular Rings Section 9, Reference, loading, and load terms #21. Formulas for moments, loads, and deformations and some selected numerical values. Ring rotating at angular rate ω rad/s about an axis perpendicular to the plane of the ring. Note the requirement of symmetry of the cross section. |
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