999 resultados para Harvard University. Class of 1877
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John Pierce kept this journal while he was a student at Harvard College. It consists of manuscript musical scores with annotations indicating the occasions at which the music was performed. These occasions included commencements, public exhibitions and Dudleian lectures. A note indicates that one anthem was prepared by Samuel Holyoke at Pierce's request, to be performed at Pierce's class commencement exercises, held on July 13, 1793. Several annotations were made in May 1794, the year following Pierce's graduation. There is a table of contents on the last page.
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This folder contains a notebook that includes handwritten copies of Kirkland's letter of resignation addressed to the Corporation of Harvard University, March 28, 1828; an address of President Kirkland to the students, delivered in the College Chapel after morning prayers, April 1, 1828; a letter from Francis C. Gray accompanied by a vote of the Corporation, April 2, 1828; a letter from Mr. Gray and vote of the Corporation, April 4, 1828; President Kirkland's reply to Mr. Gray, April 5, 1828; the address of the senior class to the President, presented to him the morning after he took leave of the College, April 2, 1828; and an address of the immediate government to Kirkland, April 2, 1828.
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1916 v.2
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1917 v.3
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1913 v.1
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S'analitza la coautoria de la UPC amb autors vinculats a institucions acadèmiques dels Estats Units, per totes les àrees temàtiques i sense considerar límits cronològics o documentals.
Resumo:
In recent years, there has been continuing interest in the participation of university research groups in space technology studies by means of their own microsatellites. The involvement in such projects has some inherent challenges, such as limited budget and facilities. Also, due to the fact that the main objective of these projects is for educational purposes, usually there are uncertainties regarding their in orbit mission and scientific payloads at the early phases of the project. On the other hand, there are predetermined limitations for their mass and volume budgets owing to the fact that most of them are launched as an auxiliary payload in which the launch cost is reduced considerably. The satellite structure subsystem is the one which is most affected by the launcher constraints. This can affect different aspects, including dimensions, strength and frequency requirements. In this paper, the main focus is on developing a structural design sizing tool containing not only the primary structures properties as variables but also the system level variables such as payload mass budget and satellite total mass and dimensions. This approach enables the design team to obtain better insight into the design in an extended design envelope. The structural design sizing tool is based on analytical structural design formulas and appropriate assumptions including both static and dynamic models of the satellite. Finally, a Genetic Algorithm (GA) multiobjective optimization is applied to the design space. The result is a Pareto-optimal based on two objectives, minimum satellite total mass and maximum payload mass budget, which gives a useful insight to the design team at the early phases of the design.