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amplifier amplitude angle angles of attack approximation assumed atmospheric axial blower axis bending blades bolt coefficient column of fresh combustion COMMITTEE FOR AERONAUTICS compensation compression condensation shock wave condensation wave condition conical nozzle constant corresponding cross section curve cycle determined diagram diameter displacement double shear Joints duraluminum effect ellipse equation exhaust end flight speed flow form drag frcm frequency fresh charge given gives increase inlet intake period investigation jet tube lead limit of proportionality load distribution Mach's method NATIONAL ADVISORY COMMITTEE nondimensional nonlinear deformations obtained Paul Schmidt percent plate proportional limit rarefaction wave reference reflected resistance rivet loads rods series of tapered shear stresses shown in figure step-curve stiffness straps structure supercharger tapered wings tests thermal lag tion turbulence valves vector velocity fluctuations velocity of sound voltage fluctuations voltmeter vortex sound Wave propagation wing with fuselage wire