Aircraft Structures
by David J. Peery · McGraw-Hill
Classic 1950 textbook on the stress analysis of aircraft structures, covering beams, thin-walled sections, shear flow, torsion of closed cells, and buckling of sheet-stringer panels. Readers learn the hand-calculation methods behind wing and fuselage structural design.
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Practitioner handbook from a former Lockheed structures engineer. It covers design loads, materials, wing, fuselage and empennage component design, joints, cutouts, fatigue and damage tolerance, and weight-efficient detail design, using tables, charts and example sizing calculations. Where Bruhn covers analysis, Niu covers design: how real wings and fuselages are laid out and detailed for fatigue and damage tolerance.
Analysis and Design of Flight Vehicle Structures
Industry reference for sizing airframe and space-vehicle structures, drawn mostly from NACA reports and full of worked numerical examples. Covers section properties, torsion, bending and shear stresses, beam web design, column and plate buckling, crippling, joints, and fatigue. Unmatched practical sizing methods (crippling, tension-field webs, lug analysis) that academic texts skip.
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