TECHNIQUES FOR PREDICTING LOCALIZED VIBRATORY ENVIRONMENTS OF ROCKET VEHICLES
Prediction of rocket vehicle environment - statistical analyses of structural configuration in vibration
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Prediction of rocket vehicle environment - statistical analyses of structural configuration in vibration
Differential linear energy spectra of a flare- produced proton beam compared with a neutron- produced recoil proton and a monoenergetic proton
Impingement electropolishing is accomplished by use of an electrolyte film, which is evenly distributed by an insulated nozzle designed to match the contour of the workpiece to be treated. The workpiece is connected to the positive terminal of a generator and the nozzle to the negative terminal.
Prediction of acoustic vibration response of rocket vehicle structures
Heat transfer and average friction coefficients for hydrogen and helium flowing in tungsten tube
Effects of ion bombardment of embryonic sites on wing growth of confused flour beetle
Comparison of specific gravity of tektites from australia, asia, texas, and czechoslovakia
Effect of electric stimulation on spinocervical tract of cat
Ordinary differential equations for stress analysis of thin spherical shells for initial pressurization
Supersonic wind tunnel tests of turbulent skin friction on flat plate at very high Reynolds number
Impact of space and space-related activities on industry and general economy of Boulder, Colorado
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Wind tunnel studies of six cones for pressure probes to determine Mach number, total pressure and flow angles
Cyclic plastic stresses in notched aluminum alloy sheets under constant-amplitude repeated tension and reversed loading - fatigue life data
Heat transfer coefficients of steam condensation in vertical downflow with liquid-vapor interface inside small tube-type condenser
Overheating in convergent section of Aerobee rocket combustion chamber nozzle due to nozzle design and regenerative cooling system
Device to measure turbulent flows by cross correlation of optical signals
Axially symmetric dynamic response solutions for cylinders subjected to pressure transients arising in propulsion systems