Cooled baffle development for M-1 engine using a subscale rocket engine
Film and transpiration cooled baffles for M-1 engine
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Film and transpiration cooled baffles for M-1 engine
Liquid flow into baffled spherical tank during weightlessness
Stability effects of several injector face baffle configurations on screech in hydrogen-oxygen rocket
Tensile testing, optical and electron fractography, conductivity testing, and chemical analysis of structural failure of oxidizer tank ring baffle web
Light radiation direction indicator with baffle of two parallel grids
Circular baffle mounted above flat-bottomed cylindrical tank outlet, discussing effect on remaining tank fluid volume and flow behavior under low gravity conditions
Acoustic behavior of baffled combustion chambers
Effect of outlet baffling on liquid residuals for outflow from cylinders in weightlessness
Dielectrophoretic baffling to control vapor ingestion in weightlessness
User manual for computer programs to determine high frequency instability in baffled annular liquid propellant rocket engines - Vol. 2
High frequency nonlinear combustion instability in baffled annular liquid propellant rocket engines - Vol. 1
Flexible ring slosh damping baffle for spacecraft fuel tank
Analysis of aluminum and nonmetallic baffles for use with oxygen containers to prevent sloshing
Variational-iterational technique for predicting wave motion and instability frequencies in baffled combustion chambers
Liquid sloshing in liquid propellant containing orbiting vehicle stabilized by active control system, examining expression for ring baffle slosh damping under reduced gravity
Electrically-grounded "optically tight' baffle installed downstream from conventional metal screen prevents discharge from entering test chamber and disturbing test process.
The radiation resistance of a beam is theoretically determined from the total acoustic power radiated into the farfield. The beam is supported in an infinite baffle, with both hinged and clamped supports considered. Asymptotic solutions are derived for frequencies well below the critical frequency. Curves, covering the entire frequency range between the low- and high-frequency asymptotic solutions, are obtained through numerical integration for the first ten modes of beams with various width-to-length ratios. For frequencies well below the critical frequency, the ratio of the radiation resistance of a beam clamped at each end to that of a beam hinged at each end is 0.851 for the first mode, 0.711 for the second mode, and asymptotically approaches 2 as the mode number tends to infinity. For both hinged and clamped supports, the radiation resistance of all modes increases with the beam width-to-length ratio.
An experimental investigation of isothermal liquid inflow patterns in a spherical container during weightlessness was conducted in a 2.2-Second Zero-Gravity Facility. The test liquids employed exhibited an essentially zero-degree static contact angle on the surface of the container. Qualitative results are presented for both baffled and unbaffled containers describing the uniformity of tank wall wetting and the liquid loss through two symmetrically located vents.