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Lecture note on the Simplex Method

Template de projeto de pesquisa nos padrões do edital universal CNPq.

This is a quick Bio Sheet I created for a D&D campaign I was playing. It uses a polish brochure template that I edited. I forgot where I got that from but if someone recognizes it, please let me know and I shall credit the right source. image credit: Rob-joseph/Deviantart

This is a LaTeX template (version from 2016 Feb. 17) for preparing documents for All-Russian Scientific Conference of the Mathematical Modeling and Boundary Value Problems [Matem. Mod. Kraev. Zadachi, Samara, Russian Federation]. It was submitted by an author writing for the 10th All-Russian Scientific Conference with international participation (MMiKZ’16). The various components of your paper [title, text, heads, etc.] are already defined on the style sheet, as illustrated by the portions given in this document. Author: Mikhail N. Saushkin (msaushkin@gmail.com) License: Creative Commons CC BY 4.0

An overview of the Cantor Set and its connection to counting.

Example report for the MNR lab

A lab report template in Russian. Шаблон отчёта по лабораторным работам (Версия от 15.02.2016) предназначен для использования студентами каф. ПМиИ СамГТУ при оформлении отчетов по лабораторным работам. Для настройки пакета listigs использовался материал статьи Михаила Конника aka virens [http://mydebianblog.blogspot.ru/2012/12/latex.html] Copyright (c) 2016 by Mikhail Saushkin (msaushkin@gmail.com) All rights reserved except the rights granted by the Creative Commons Attribution 4.0 International Licence

This simulation plan aims to explain and document all steps to be taken in the simulation analysis of the Fokker-100 case. This case is the scenario in which the aircraft touches the ground during landing, introducing loads on the landing gear. The landing gear consists of 2 rear gears around mid-span and one in the front. Furthermore, the pilot uses the rudder which induces a lateral force on the tail. As stated in the assignment, it is required to find the maximum normal stress and location of this in the fuselage, the maximum shear stress and its location in the fuselage, and the maximum shear flow in the frames that introduce the loads from the landing gears into the fuselage.

Chicago Style History Paper which includes figures with \usepackage{wrapfig} and \begin{wrapfigure}