Bimetallic devices for stirring fluids

Device consists of helical heating coil inside cylinder and affixed at one end. Piston is fastened at other end and is free to move axially through cylinder. Electrical power extends coil when applied to conductors. Bimetallic stirrer may also be made in vane form

Shock-layer radiation measurement

Method and apparatus for measuring shock layer radiation distribution about high velocity object

Bimetallic fluid displacement apparatus

Stirring and heating stored gases and liquids is accomplished by using the deformation of a bimetallic structure which deforms significantly when heated. The deformation is used to effect gradual or impulsive motion of a piston, vane, wire, or diaphram for displacement of the fluid. The heated bimetallic is also employed for heating the stored fluid

Convective and radiative heat transfer during reentry and advanced techniques for their simulation

Convective and radiative heat transfer during reentry simulatio

Creating a Climate to Realize Institutional Diversification Goals: A Phenomenological Study of Campus Diversification Best Practices

This study investigates the diversification plans and goals of four university or college campuses in California examining the insight and perspectives of their respective administrators. Diversification of the institution has been adopted as a strategic plan or mission goal. The investigation analyzes the strides made toward the goal by investigating the efforts of the institutions in the intercultural training of current staff and faculty. Where best practices for diversification of the institution at every level exist, I will review what is being done and contrast those findings with institutions where a diversification goal exists, but training programs for staff members fall short of industry and scholarly recommendations. An initial literature review shows few works dedicated to staff training in the intercultural arena for such institutions. My final goal is to identify best practices when they exist and examine the gaps in training that institutions may face

Investigation in the Ames Supersonic Free-Flight Wind Tunnel of the Static Longitudinal Stability of the Hermes A-3B Missile at a Mach Number of 5.0

Models of the Hermes A-3B missile were tested in the Ames supersonic free-flight wind tunnel to determine the static-longitudinal-stability characteristics at a Mach number of 5.0 and a Reynolds number based on body length of 10 million. The results indicated that the model center of pressure was 45.3 percent of the body length aft of the nose and the lift-curve slope based on body frontal area was 0.064 per degree. Estimates indicated that the effect on these characteristics of aeroelastic twisting of the model fins was small but important if a precise location of center of pressure is required. A comparison of the test results with predictions based on available theory showed that the theory was useful only for rough estimates, The drag coefficient at zero lift, based on body frontal area, was found to be 0.155