Wing loading design

Article Abstract:

Higher wing loadings result in smaller, faster and stronger aircraft at the expense of higher stall and landing speeds. Spins, snaprolls and avalanches, which involve wing stalling, are easier to enter. Proper loading can enhance performance.

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Stressed skin design

Article Abstract:

Step-by-step instructions are presented for the stressed skin structure of the 'Swift' model airplane. Details are provided on wings, fuselage and landing gear as well as a simple technique for estimating weight.

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Stressed skin design

Article Abstract:

Structural material should be located as far as possible from the neutral axis to maximize strength/weight ratios. Tension, compression, shear and leverage are the forces with which to contend.

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