Aeroplane construction and operation; including notes on aeroplane design and aerodynamic calculation, materials, etc. A comprehensive illustrated manual of instruction for aeroplane constructors, aviators, aero-mechanics, flight officers and students. Adapted either for schools or home study (1918)
Rathbun, John B · Chicago : Stanton and Van Vliet Co. · leaf 270
can be designed so that they are adjustable tochanges in the section of the longitudinals. In one ma-chine, the width and depth of the longitudinals are kept FUSELAGE DETAILS 261 constant, the variation in weight and section being accom-plished by increasing the depth of the channelling as therear… … rrG.S>^^ FJ&2&B ne.23-C^ -^^ Figs. 27-28-29-30. Fuselage Framing Members and Details. by chamfering, as shown by Fig. 28. If the width andthickness is maintained, much of the interior material canbe removed without danger of reducing the strength.Sketch (A) in Fig. 28 shows a very common…
Airplanes
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