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External Ballistics Primer for Engineers Part I: Aerodynamics & Projectile Motion
402.pdf A SunCam online continuing education course External Ballistics Primer for Engineers Part I: Aerodynamics & Projectile Motion by Terry A. Willemin, P.E. 402.pdf External Ballistics Primer for Engineers A SunCam online continuing education course Introduction This primer covers basic aerodynamics, fluid mechanics, and flight-path modifying factors as they relate to ballistic projectiles. To the unacquainted, this could sound like a very focused or unlikely topic for most professional engineers, and might even conjure ideas of guns, explosions, ICBM’s and so on. But, ballistics is both the science of the motion of projectiles in flight, and the flight characteristics of a projectile (1). A slightly deeper dive reveals the physics behind it are the same that engineers of many disciplines deal with regularly. This course presents a conceptual description of the associated mechanics, augmented by simplified algebraic equations to clarify understanding of the topics. Mentions are made of some governing equations with focus given to a few specialized cases. This is not an instructional tool for determining rocket flight paths, or a guide for long-range shooting, and it does not offer detailed information on astrodynamics or orbital mechanics. The primer has been broken into two modules or parts. This first part deals with various aerodynamic effects, earth’s planetary effects, some stabilization methods, and projectile motion as they each affect a projectile’s flight path. In part II some of the more elementary measurement tools a research engineer may use are addressed and a chapter is included on the ballistic pendulum, just for fun. Because this is introductory course some of the sections are laconic/abridged touches on the matter; however, as mentioned, they carry application to a broad spectrum of engineering work. -
Approximate Analytical Description of the Projectile Motion with a Quadratic Drag Force
Athens Journal of Sciences- Volume 1, Issue 2 – Pages 97-106 Approximate Analytical Description of the Projectile Motion with a Quadratic Drag Force By Peter Chudinov In this paper, the problem of the motion of a projectile thrown at an angle to the horizon is studied. With zero air drag force, the analytic solution is well known. The trajectory of the projectile is a parabola. In situations of practical interest, such as throwing a ball with the occurrence of the impact of the medium the quadratic resistance law is usually used. In that case the problem probably does not have an exact analytic solution and therefore in most scientific publications it is solved numerically. Analytic approaches to the solution of the problem are not sufficiently advanced. Meanwhile, analytical solutions are very convenient for a straightforward adaptation to applied problems and are especially useful for a qualitative analysis. That is why the description of the projectile motion with a simple approximate analytical formula under the quadratic air resistance represents great methodological interest. Lately these formulas have been obtained. These formulas allow us to obtain a complete analytical description of the problem. This description includes analytical formulas for determining the basic eight parameters of projectile motion. Analytical formulas have been derived for the six basic functional dependences of the problem, including the trajectory equation in Cartesian coordinates. Also this description includes the determination of the optimum throwing angle and maximum range of the motion. In the absence of air resistance, all these relations turn into well-known formulas of the theory of the parabolic motion of the projectile. -
A STUDY of CANNON-FIRED, ROCKET-ASSISTED PROJECTILE TRAJECTORIES Dy Donald E. Kenney. a Thesis Submitted to the Faculty of the D
A study of cannon-fired, rocket- assisted projectile trajectories Item Type text; Thesis-Reproduction (electronic) Authors Kenney, Donald Edwin, 1927- Publisher The University of Arizona. Rights Copyright © is held by the author. Digital access to this material is made possible by the University Libraries, University of Arizona. Further transmission, reproduction or presentation (such as public display or performance) of protected items is prohibited except with permission of the author. Download date 28/09/2021 17:49:26 Link to Item http://hdl.handle.net/10150/319828 A STUDY OF CANNON-FIRED, ROCKET-ASSISTED PROJECTILE TRAJECTORIES Dy Donald E. Kenney. A Thesis Submitted to the Faculty of the DEPARTMENT OF AEROSPACE AND MECHANICAL ENGINEERING . In' Partial Fulfillment of the Requirement For the Degree of MASTER OF SCIENCE In the Graduate College THE UNIVERSITY OF ARIZONA 1964 STATEMENT BY AUTHOR This thesis has been submitted in partial ful fillment of requirements for an advanced degree at The University of Arizona and is deposited in the University library to be made available to borrowers under rules of the library. Brief quotations from this thesis are allowable without special permission, provided that accurate ac knowledgment of source is made. Requests for permission for extended quotation from or reproduction of this manu script in whole or in part may be granted by the head of the major department or the Dean of the Graduate College when in his judgment the proposed use of the material is in the interests of scholarship. In all other instances, however, permission must be obtained from the author. SIGNED: APPROVAL BY THESIS DIRECTOR This thesis has been approved on the date shown below: oyrza*? [/\a A /Lw v/ ^ THOMAS L. -
Numerical Solution to a Nonlinear External Ballistics Model for a Direct Fire Control System
Numerical Solution to a Nonlinear External Ballistics Model for a Direct Fire Control System MARTIN SKANDE Master of Science Thesis Stockholm, Sweden 2014 Numerical Solution to a Nonlinear External Ballistics Model for a Direct Fire Control System Martin Skande Master of Science Thesis MMK 2014:58 MDA 487 KTH Industrial Engineering and Management Machine Design SE-100 44 STOCKHOLM Examensarbete MMK 2014:58 MDA 487 Numerisk Lösning för en Olinjär Ytterballistik till ett Direkt Eldledningssystem Martin Skande Godkänt Examinator Handledare 2014-06-26 Jan Wikander Bengt O. Eriksson Uppdragsgivare Kontaktperson Fredrik Lundh Daniel Hellberg Sammanfattning Detta examensarbete är en utvecklings- och evalueringsprocess av en numeriskt löst ytterballistik modell för ett eldledningssystem utvecklat av SAAB Technologies. Den befintliga ballistik modell som används av eldledningssystemet idag är linjäriserad vilket simplifierar problemet att nå upp till de hårda realtidskrav som finns, dock på grund av de approximationer och simplifieringar knutna till linjäriseringen finns det utrymme för förbättringar i termer av beräkningsnoggrannhet. Ökande krav på systemnivå prestanda tillsammans med initiala utredningar motiverade en undersökning av en numeriskt löst ytterballistik i termer av prestanda relativt den befintliga linjäriserade ytterballistik modellen. Examensarbetet har fokuserat på hela processen från första koncept av en numeriskt löst ytterballistik modell ända till implementering på eldledningssystemet. Arbetet är grundat i ett teoretiskt ramverk i huvudsak inriktat på ballistikteori. Konceptet som har tagits fram använder en olinjär ytterballistikmodell baserad på en befintlig modell beskriven i teori och löses med hjälp av en fjärde ordningens Runge-Kutta integrator. En iterativ metod liknande en diskret kontrollstruktur används för att finna initial- och ändvärden till ballistikmodellen och en adaptiv steglängdsalgoritm används som klarar av att upprätthålla realtidskraven. -
Aristotle, Projectiles and Guns Stephen M
Aristotle, projectiles and guns Stephen M. Walley* SMF Fracture and Shock Physics Group, The Cavendish Laboratory, J.J. Thomson Avenue, Cambridge, CB3 0HE, UK Abstract When guns were developed in Europe in the 14th century, the theory of projectile motion was not the one we are familiar with today due to Galileo and Newton but the one taught by Aristotle approximately 1700 years earlier. In addition to Aristotle’s wide-ranging philosophical concerns, his theory arose from the observation in everyday life that if an object is moving something must be moving it. This idea works very well for the horse and cart but is puzzling if you apply it to a thrown stone or spear. Problems with Aristotle’s theory of projectile motion were identified by one or two people between his time and the 14th century, particularly John Philoponus (6th century AD) and John Buridan (14th century AD). An archer or a spearman does not need a theory of projectile motion, just a great deal of practice. But once the gun was invented it became important to know what angle a barrel should be oriented at and how much propellant to use, particularly as gunpowder was expensive. However, for many years afterwards the manufacturing techniques used meant that cannonballs were a loose fit to gun-barrels making cannons both inaccurate and of poor reproducibility shot-to-shot. Also air resistance makes the trajectory both impossible to calculate and qualitatively similar to theories based on Aristotle’s writings. It was not until Galileo and Newton worked on the problem that a better theory of ideal projectile motion was arrived at.