Wind Tunnel Test of the Conversion Process of a Folding Tilt-Rotor Aircraft Using a Semispan Unpowered Model. Volume 4. Part 2. Blade Stress Analysis, Bench Tests, and Wind Tunnel Model Details
BOEING VERTOL CO PHILADELPHIA PA
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The document presents the detailed results of the blade stress analysis and the bench tests, as well as a description of the wind tunnel and the model. Mathematical findings are given in developed equations and in voluminous tabular data. Additional information is provided in the form of engineering graphs and curves, schematic diagrams, and photographs of the model and test setup. This volume is actually an appendix to Part I, Analysis and Results.