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- Creators: Barrett, The Honors College
- Creators: Department of Physics
Description
Research has shown that English language development among L2 learners can be greatly enhanced through at-home parental involvement. However, few pieces of research have studied how parents involve themselves in their child’s English education. In this study, questions revolving around the parents’ level of involvement with their child’s English education are addressed to help analyze what Taiwanese parents are doing to enhance or hinder their child’s language-learning growth. Through the questionnaire data provided by forty-four of parental respondents, results suggest that parents’ involvement efforts are often not considered proportional to the child’s English educational success. Solutions to help parents nurture effective academic growth in children’s English learning endeavors are discussed to help parents better approach English educational involvement.
ContributorsFischer, Nathan (Author) / Matsuda, Aya (Thesis director) / Manalo, Emmanuel (Committee member) / Barrett, The Honors College (Contributor) / School of International Letters and Cultures (Contributor) / Department of Physics (Contributor)
Created2022-05
Description
This thesis examines how a recently proposed concept for a highly-truncated aerospike nozzle
can be expected to perform at altitudes corresponding to ambient pressures from sea-level to
full vacuum conditions, as would occur during second-stage ascent and during second-stage
descent and return to Earth. Of particular importance is how the base pressure varies with
ambient pressure, especially at low ambient pressures for which the resulting highly underexpanded flows exiting from discrete thrust chambers around the truncated aerospike merge to
create a closed (unventilated) base flow. The objective was to develop an approximate but
usefully accurate and technically rooted way of estimating conditions for which the jets issuing
from adjacent thrust chambers will merge before the end of the truncated aerospike is reached.
Three main factors that determine the merging distance are the chamber pressure, the altitude,
and the spacing between adjacent thrust chambers. The Prandtl-Meyer expansion angle was
used to approximate the initial expansion of the jet flow issuing from each thrust chamber.
From this an approximate criterion was developed for the downstream distance at which the
jet flows from adjacent thrust chambers merge. Variations in atmospheric gas composition,
specific heat ratio, temperature, and pressure with altitude from sea-level to 600 km were
accounted for. Results showed that with decreasing atmospheric pressure during vehicle
ascent, the merging distance decreases as the jet flows become increasingly under-expanded.
Increasing the number of thrust chambers decreases the merging distance exponentially, and
increasing chamber pressure results in a decrease of the merging distance as well.
ContributorsHerrington, Katie (Author) / Dahm, Werner (Thesis director) / Takahashi, Timothy (Committee member) / Barrett, The Honors College (Contributor) / Mechanical and Aerospace Engineering Program (Contributor) / Department of Physics (Contributor)
Created2024-05