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PAPERS APPEARING IN PART
STATEOFTHEART ASSESSMENT OF MOBILITY MEASUREMENTS A SUMMARY
DEPARTMENT OF DEFENSE POLICY ON RELIABILITY AND MAINTAINABILITY
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acceleration accelerometers acoustic active damper aircraft amplitude analysis applied approximately beam blade calculated Center chamber complex modulus configuration conservatism constant criteria curve cylinder damping damping factors deformation degrees of freedom developed displacement dynamic effect eigenvalue elastic Engineering equation equipment error evaluate excitation experimental explosive factor finite element model flight Flight Dynamics force Fourier Fourier transform hull impact impulse input Laboratory linear loading locations material matrix measured ment method missile modal modal loss mode shapes modulus motion mounted NASTRAN natural frequency node normal obtained parameters peak plots predicted pressure problem pulse quency random variables ratio response shaker shell Shock and Vibration shock test shown in Figure simulation skyhook solution spectra spray Steel Mosquito stiffness strain stress structure surface Table target technique tion transfer function tube U.S. Army vector velocity viscoelastic wave Wright-Patterson AFB