Engineering topics
Publications and source records attributed to Bui, T..
Stratospheric hydration and dehydration were measured inside the Arctic polar vortex in January and February 2000, as part of the Sage III Ozone Loss Validation Experiment (SOLVE).
This work describes aircraft-based lidar observations of thin cirrus clouds at the tropical tropopause in the central Pacific obtained during the Tropical Ozone Transport Experiment/Vortex Ozone Transport Experiment (TOTE/VOTE) in December 1995 and February 1996.
On 8 May 1997 vertical profiles of over 30 different gases were measured remotely in solar occultation by the JPl MkIV Interferometer during a balloon flight launched from Fairbanks, Alaska.
With aircraft-mounted in-situ and remote sensing instruments for dynamical, thermal, and chemical measurements, we studied two cases of tropopause folding.
A new technique is presented to determine the degree of denitrification that occured during the 1996/97 Arctic winter, based on balloon and aircraft borne measurements of NOy, N2O and CH4. In this study high-altitude balloon measurements are used to define the properties of air masses that later descend in the polar vortex to altitudes sampled by the ER-2 aircraft and mix isentropically with mid-latitude air.
The entrainment time scale in our study is considerably less than the value found by a similar study that focused on observations obtained in the lower stratosphere during 1994.
This study comprised direct thrust measurements, flow visualization by use of a spark shadowgraph technique, and mean and fluctuating velocity measurements with a pitot tube and linearized constant temperature hot-wire anemometry respectively. A gain in thrust of as much as 10 to 15% was observed for the pulsatile ejector flow as compared to the steady flow configuration. From the velocity profile measurements, it is concluded that this enhanced augmentation for pulsatile flow as compared to a nonpulsatile one was accomplished by a corresponding increased entrainment by the primary jet flow. It is also concluded that the augmentation and total entrainment by a constant area ejector critically depends upon the inlet geometry of the ejector. Experiments were performed to evaluate the influence of primary jet to ejector area ratio, ejector length, and presence of a diffuser on pulsatile ejector performance.