Transient pressure measuring methods research Final summary technical report
Transient pressure measuring methods as applied to liquid propellant rocket thrust chamber
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Transient pressure measuring methods as applied to liquid propellant rocket thrust chamber
Finite difference method to obtain numerical results on normal shock wave diffraction by sphere and subsequent transient flow
Numerical method for treating time transient gas lubrication equation
Numerical method for determining transient blade motions of rotor with flapping and lead-lag degrees of freedom
Transient heat conduction in finite slabs with position dependent heat generation
Transient radiation and conduction in slotted slab and hollow cylinder
Numerical digital computer method for determining transient responses of nonlinear automatic systems based on calculation of convolution integral
Steady state and transient full-scale, half-scale and quarter-scale thermal models in simulated space environment
Transient heat transfer and thermal stresses for nuclear rocket due to sudden hydrogen coolant flow increase
Ignition pressure transient in solid rocket motors, examining chamber filling interval, flame propagation, heat transfer correlation, burning area, etc
Transient heat transfer analysis of Apollo Service Module
Instrumenting techniques for models under aerodynamic transient heating
Transient heat transfer through monatomic collisionless ideal gas enclosed between parallel walls analyzed for step change in one wall temperature
Transient temperature distribution of cylinder subject to radiation cooling, giving dimensionless computer-derived graphs
Transient radiation of electric dipole in uniaxially anisotropic plasma examined for signal frequency greater and less than plasma frequency
Satellite synthetic aperture radar interferometry reveals transient strain accumulation along the Blackwater-Little Lake fault system within the Eastern California shear zone.
Power MOSFET devices are susceptible to heavy-ion induced Single-Event Gate Rupture. Computer modeling show that intense electric field transients can trigger the SEGR phenomenon.
The conservatism and overtest indices measured for multiple transient and SRS tests and a least favorable response test are compared to those of a swept-sine test for a typical spacecraft component.