Transient pressure measurements in liquid propellant rocket thrust chambers.
Transient pressure measurements in rocket thrust chambers used in propulsion systems research
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Transient pressure measurements in rocket thrust chambers used in propulsion systems research
Testing method for spacecraft response during environmental testing equivalent to its response to excitation by sinusoidal transients in flight
Steady state and transient full-scale, half-scale and quarter-scale thermal models in simulated space environment
Variation method applied to transient thermal conductivity in semiinfinite slab with nonlinear boundary condition
Transient currents and voltages in breaking electric contacts in low voltage inductive circuits - electrode erosion
Evaluation capabilities for transient pressure transducers
Transient pressure transducers for measuring dynamic pressures in rocket thrust chambers
Transient heat transfer film coefficients for gas flow in tube
Transient response from Liapunov stability equation
Heat transfer across metal surfaces under transient temperature and pressure environment
Axially symmetric dynamic response solutions for cylinders subjected to pressure transients arising in propulsion systems
Users manual for general purpose digital computer program for predicting dynamic response of cylinders subjected to ramp and sinusoidal pressure transients
Transient heat transfer between thin circular tube and incompressible fluid, considering radial conduction and heat loss
Ignition pressure transient of rocket motor, discussing initial ignition event, flame spreading and final chamber filling, convective heating effect on burning rate, etc
Transient resonant response of inhomogeneously broadened nuclear spin system to pulsed electromagnetic field represented as series of Bessel functions modulated by time-varying coefficients
Heat transfer across surfaces in contact - effects of transient temperature and pressure environments
Transient radiation effects on reactor thermocouples
Evaluation of transient loads for environmental testing of spacecraft using multiple degree of freedom model