Aeronautical Science 101: the Development of Engineering Science in Aeronautical Engineering Education at the University of Minnesota
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Introduction to Aircraft Aeroelasticity and Loads
JWBK209-FM-I JWBK209-Wright November 14, 2007 2:58 Char Count= 0 Introduction to Aircraft Aeroelasticity and Loads Jan R. Wright University of Manchester and J2W Consulting Ltd, UK Jonathan E. Cooper University of Liverpool, UK iii JWBK209-FM-I JWBK209-Wright November 14, 2007 2:58 Char Count= 0 Introduction to Aircraft Aeroelasticity and Loads i JWBK209-FM-I JWBK209-Wright November 14, 2007 2:58 Char Count= 0 ii JWBK209-FM-I JWBK209-Wright November 14, 2007 2:58 Char Count= 0 Introduction to Aircraft Aeroelasticity and Loads Jan R. Wright University of Manchester and J2W Consulting Ltd, UK Jonathan E. Cooper University of Liverpool, UK iii JWBK209-FM-I JWBK209-Wright November 14, 2007 2:58 Char Count= 0 Copyright C 2007 John Wiley & Sons Ltd, The Atrium, Southern Gate, Chichester, West Sussex PO19 8SQ, England Telephone (+44) 1243 779777 Email (for orders and customer service enquiries): [email protected] Visit our Home Page on www.wileyeurope.com or www.wiley.com All Rights Reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted in any form or by any means, electronic, mechanical, photocopying, recording, scanning or otherwise, except under the terms of the Copyright, Designs and Patents Act 1988 or under the terms of a licence issued by the Copyright Licensing Agency Ltd, 90 Tottenham Court Road, London W1T 4LP, UK, without the permission in writing of the Publisher. Requests to the Publisher should be addressed to the Permissions Department, John Wiley & Sons Ltd, The Atrium, Southern Gate, Chichester, West Sussex PO19 8SQ, England, or emailed to [email protected], or faxed to (+44) 1243 770620. -
Thermodynamic Physics and the Poetry and Prose of Gerard Manley Hopkins
Georgia State University ScholarWorks @ Georgia State University English Dissertations Department of English 5-11-2015 Literatures of Stress: Thermodynamic Physics and the Poetry and Prose of Gerard Manley Hopkins Thomas Mapes Follow this and additional works at: https://scholarworks.gsu.edu/english_diss Recommended Citation Mapes, Thomas, "Literatures of Stress: Thermodynamic Physics and the Poetry and Prose of Gerard Manley Hopkins." Dissertation, Georgia State University, 2015. https://scholarworks.gsu.edu/english_diss/134 This Dissertation is brought to you for free and open access by the Department of English at ScholarWorks @ Georgia State University. It has been accepted for inclusion in English Dissertations by an authorized administrator of ScholarWorks @ Georgia State University. For more information, please contact [email protected]. LITERATURES OF STRESS: THERMODYNAMIC PHYSICS AND THE POETRY AND PROSE OF GERARD MANLEY HOPKINS by THOMAS MAPES Under the Direction of Paul Schmidt, PhD ABSTRACT This dissertation examines two of the various literatures of energy in Victorian Britain: the scientific literature of the North British school of energy physics, and the poetic and prose literature of Gerard Manley Hopkins. As an interdisciplinary effort, it is intended for several audiences. For readers interested in science history, it offers a history of two terms – stress and strain – central to modern physics. As well, in discussing the ideas of various scientific authors (primarily William John Macquorn Rankine, William Thomson, P.G. Tait, and James Clerk Maxwell), it indicates several contributions these figures made to larger culture. For readers of Hopkins’ poems and prose, this dissertation corresponds with a recent trend in criticism in its estimation of Hopkins as a scientifically informed writer, at least in his years post-Stonyhurst. -
CHAPTER TWO - Static Aeroelasticity – Unswept Wing Structural Loads and Performance 21 2.1 Background
Static aeroelasticity – structural loads and performance CHAPTER TWO - Static Aeroelasticity – Unswept wing structural loads and performance 21 2.1 Background ........................................................................................................................... 21 2.1.2 Scope and purpose ....................................................................................................................... 21 2.1.2 The structures enterprise and its relation to aeroelasticity ............................................................ 22 2.1.3 The evolution of aircraft wing structures-form follows function ................................................ 24 2.2 Analytical modeling............................................................................................................... 30 2.2.1 The typical section, the flying door and Rayleigh-Ritz idealizations ................................................ 31 2.2.2 – Functional diagrams and operators – modeling the aeroelastic feedback process ....................... 33 2.3 Matrix structural analysis – stiffness matrices and strain energy .......................................... 34 2.4 An example - Construction of a structural stiffness matrix – the shear center concept ........ 38 2.5 Subsonic aerodynamics - fundamentals ................................................................................ 40 2.5.1 Reference points – the center of pressure..................................................................................... 44 2.5.2 A different -
Introduction to Aeroelasticity.Pdf
Aeroelasticity Dr. Ugur GUVEN Aerospace Engineer (P.hD) Nuclear Science and Technology Engineer (M.Sc) What is Aeroelasticity • Aeroelasticity is broadly defined as the interaction between the aerodynamic forces and the structural forces causing a deformation in the structure of the aerospace craft as well as in its control mechanism or in its propulsion systems. Importance of Aeroelasticity • Aeroelasticity has become a very important force especially after the 1950’s. • The interaction between aerodynamic loads and structural deformations have gained great importance in view of factors related to the design of aircraft as well as missiles. • Aeroelasticity plays at least some part on fuel sloshing as well as on the reentry of spacecraft in astronautics. Trends in Technology • Due to the advancements in technology, it has become quite common to see the slenderness ratio (ratio of length of wing span to thickness at the root) increase. • The wing span area as well as the length of aircrafts have increased causing aircraft to become much more susceptible to interaction between structural loads and aerodynamic loads Slenderness Ratio Effect of Aerodynamic Loads • The forces of lift and drag as well as torsion moment will have some sort of effect on the structural integrity of the spacecraft. • In many cases, some parts of aircraft or spacecraft may bend or ripple slightly due to these loads. • The frequency of these loads and effects can also cause the aircraft’s structure to suffer from metal fatigue in the long run. Scope of Aeroelasticity Vibration • One of the ways in which aerodynamic and structural forces collide with each other is through vibration. -
Comparison of Theodorsen's Unsteady Aerodynamic Forces with Doublet Lattice Generalized Aerodynamic Forces 5B
NASA/TM–2017-219667 Comparison of Theodorsen’s Unsteady Aerodynamic Forces with Doublet Lattice Generalized Aerodynamic Forces Boyd Perry, III Langley Research Center, Hampton, Virginia September 2017 NASA STI Program . in Profile Since its founding, NASA has been dedicated to the x CONFERENCE PUBLICATION. advancement of aeronautics and space science. The Collected papers from scientific and technical NASA scientific and technical information (STI) conferences, symposia, seminars, or other program plays a key part in helping NASA maintain meetings sponsored or co-sponsored by NASA. this important role. x SPECIAL PUBLICATION. Scientific, The NASA STI program operates under the auspices technical, or historical information from NASA of the Agency Chief Information Officer. It collects, programs, projects, and missions, often organizes, provides for archiving, and disseminates concerned with subjects having substantial NASA’s STI. The NASA STI program provides access public interest. to the NTRS Registered and its public interface, the NASA Technical Reports Server, thus providing one x TECHNICAL TRANSLATION. of the largest collections of aeronautical and space English-language translations of foreign science STI in the world. Results are published in both scientific and technical material pertinent to non-NASA channels and by NASA in the NASA STI NASA’s mission. Report Series, which includes the following report types: Specialized services also include organizing and publishing research results, distributing x TECHNICAL PUBLICATION. Reports of specialized research announcements and feeds, completed research or a major significant phase of providing information desk and personal search research that present the results of NASA support, and enabling data exchange services. Programs and include extensive data or theoretical analysis. -
AAE556-Aeroelasticity
AIRCRAFT AEROELASTIC DESIGN AND ANALYSIS An introduction to fundamental concepts of static and dynamic aeroelasticity - with simple idealized models and mathematics to describe the essential features of aeroelastic problems. These notes are intended for the use of Purdue University students enrolled in AAE556. They are not for sale or intended for distribution to others, but may be used for educational purposes, with prior permission of the author. Terry A. Weisshaar Purdue University © 1995 (Second edition -2009) Introduction - page 1 Preface to Second Edition – The purpose and scope These notes are the result of three decades of experiences teaching a course in aeroelasticity to seniors and first or second year graduate students. During this time I have presented lectures and developed homework problems with the objective of introducing students to the complexities of a field in which several major disciplines intersect to produce major problems for high speed flight. These problems affect structural and flight stability problems, re-distribution of external aerodynamic loads and a host of other problems described in the notes. This three decade effort has been challenging, but more than anything, it has been fun. My students have had fun and have been contributors to this teaching effort. Some of them have even gone on to surpass my skills in this area and to be recognized practitioners in this area. First of all, let me emphasize what these notes are not. They are not notes on advanced methods of analysis. They are not a “how to” book describing advanced methods of analysis required to analyze complex configurations. If your job is to compute the flutter speed of a Boeing 787, you will have to learn that skill elsewhere. -
영어 우리말 a Balloon Satellite 기구 위성 a Posteriori Probability 후시
영어 우리말 a balloon satellite 기구 위성 a posteriori probability 후시(적) 확률, 사후 확률 a priori 선험- a priori distribution 선험 분포 a priori probability 선험 확률 Abbe prism 아베 프리즘, 아베 각기둥 Abbe's refractometer 아베 굴절계, 아베 꺾임 재개 Abelian group 아벨군, 아벨 무리, 가환군 aberration (1)수차 (2)광행차 abnormal birefringence 비정상 복굴절, 비정상 겹꺾임 abnormal glow discharge 비정상 글로 방전 abnormal liquid 비정상 액체 abnormal reflection 비정상 반사, 비정상 되비침 abnormal scattering 비정상 산란, 비정상 흩뜨림 A-bomb 원자 폭탄 [= atomic bomb] abrasion 마멸, 벗겨짐 abscissa 가로축, 횡축 absolute 절대- absolute ampere 절대 암페어「단위」 absolute convergence 절대 수렴 absolute counting 절대 수셈 absolute counting method 절대 수셈법 absolute differential calculus (1)절대 미분 (2)절대미분학 absolute electromagnetic unit 절대 전자기 단위 absolute electrometer 절대 전위계 absolute error 절대 오차 absolute galvanometer 절대 검류계 absolute humidity 절대 습도 absolute hygrometer 절대습도계 absolute luminosity 절대 광도 absolute magnetic well 절대 자기 우물 absolute magnitude 절대 크기 absolute measurement 절대 측정 absolute motion 절대 운동 absolute parallax 절대 시차 absolute pressure 절대 압력 absolute refractive index 절대 굴절률, 절대 꺾임률 absolute rest 절대 정지 absolute space 절대 공간 absolute system of units 절대 단위계 absolute temperature 절대 온도 absolute temperature scale 절대 온도 눈금 absolute time 절대 시간 absolute unit 절대 단위 absolute vacuum 절대 진공 absolute value 절대값 absolute viscosity 절대 점(성)도 absolute zero 절대 영도 absolute zero point 절대 영(도)점 absolute zero potential 절대 영퍼텐셜 absolutely convergent series 절대 수렴 급수 absorbance (1)흡수도 (2)흡광도 absorbancy (1)흡수도 (2)흡광도 absorbent (1)흡수제 (2)흡광제 absorber (1)흡수체, 흡수기 (2)흡광체 absorptance 흡수율 absorption (1)흡수 (2)흡광 (3)흡음 -
Fundamentals of Biomechanics Duane Knudson
Fundamentals of Biomechanics Duane Knudson Fundamentals of Biomechanics Second Edition Duane Knudson Department of Kinesiology California State University at Chico First & Normal Street Chico, CA 95929-0330 USA [email protected] Library of Congress Control Number: 2007925371 ISBN 978-0-387-49311-4 e-ISBN 978-0-387-49312-1 Printed on acid-free paper. © 2007 Springer Science+Business Media, LLC All rights reserved. This work may not be translated or copied in whole or in part without the written permission of the publisher (Springer Science+Business Media, LLC, 233 Spring Street, New York, NY 10013, USA), except for brief excerpts in connection with reviews or scholarly analysis. Use in connection with any form of information storage and retrieval, electronic adaptation, computer software, or by similar or dissimilar methodology now known or hereafter developed is forbidden. The use in this publication of trade names, trademarks, service marks and similar terms, even if they are not identified as such, is not to be taken as an expression of opinion as to whether or not they are subject to proprietary rights. 987654321 springer.com Contents Preface ix NINE FUNDAMENTALS OF BIOMECHANICS 29 Principles and Laws 29 Acknowledgments xi Nine Principles for Application of Biomechanics 30 QUALITATIVE ANALYSIS 35 PART I SUMMARY 36 INTRODUCTION REVIEW QUESTIONS 36 CHAPTER 1 KEY TERMS 37 INTRODUCTION TO BIOMECHANICS SUGGESTED READING 37 OF UMAN OVEMENT H M WEB LINKS 37 WHAT IS BIOMECHANICS?3 PART II WHY STUDY BIOMECHANICS?5 BIOLOGICAL/STRUCTURAL BASES -
A Historical Overview of Flight Flutter Testing
tV - "J -_ r -.,..3 NASA Technical Memorandum 4720 /_ _<--> A Historical Overview of Flight Flutter Testing Michael W. Kehoe October 1995 (NASA-TN-4?20) A HISTORICAL N96-14084 OVEnVIEW OF FLIGHT FLUTTER TESTING (NASA. Oryden Flight Research Center) ZO Unclas H1/05 0075823 NASA Technical Memorandum 4720 A Historical Overview of Flight Flutter Testing Michael W. Kehoe Dryden Flight Research Center Edwards, California National Aeronautics and Space Administration Office of Management Scientific and Technical Information Program 1995 SUMMARY m i This paper reviews the test techniques developed over the last several decades for flight flutter testing of aircraft. Structural excitation systems, instrumentation systems, Maximum digital data preprocessing, and parameter identification response algorithms (for frequency and damping estimates from the amplltude response data) are described. Practical experiences and example test programs illustrate the combined, integrated effectiveness of the various approaches used. Finally, com- i ments regarding the direction of future developments and Ii needs are presented. 0 Vflutte r Airspeed _c_7_ INTRODUCTION Figure 1. Von Schlippe's flight flutter test method. Aeroelastic flutter involves the unfavorable interaction of aerodynamic, elastic, and inertia forces on structures to and response data analysis. Flutter testing, however, is still produce an unstable oscillation that often results in struc- a hazardous test for several reasons. First, one still must fly tural failure. High-speed aircraft are most susceptible to close to actual flutter speeds before imminent instabilities flutter although flutter has occurred at speeds of 55 mph on can be detected. Second, subcritical damping trends can- home-built aircraft. In fact, no speed regime is truly not be accurately extrapolated to predict stability at higher immune from flutter. -
Aeroelasticity
1 Matthew Moraguez Aeroelasticity What is Aeroelasticity? An airplane’s wing generates an upward AEROELASTICITY, NOUN force, known as lift, when it passes through air. Although lift is needed for a plane to fly, A term used in the field of aerospace its effect on the structure of the plane can be engineering to describe the interaction harmful. Aeroelasticity refers to the between a structure and a moving fluid [1]. deformation of an airplane’s wing in response to aerodynamic forces, such as lift. [1] Static vs. Dynamic Aeroelasticity Aeroelastic effects are classified as either static or dynamic. While static effects reach an equilibrium, dynamic effects are defined by oscillations [2]. Static Aeroelasticity: Aeroelasticity applies to Divergence refers to a process in which the lift a wing produces causes the wing itself to twist. This twisting any situation in which a leads to greater lift, which causes more twisting. The fluid (gas or liquid) flows process continues until equilibrium is reached [1]. In around a structure [3]. order to prevent divergence, a wing must be stiff enough to prevent twisting. If the wing is too flexible or the force of lift is too strong, divergence will occur [2]. DID YOU KNOW? Aileron reversal occurs when wing twisting causes the plane’s response to the pilot’s commands to be Aeroelasticity affects airplane reversed from the expected. In other words, when a stability, bridge design, and even blood flow through the body! [3] pilot tries to turn left, the plane will turn right [2]. Dynamic Aeroelasticity: Above a critical wind speed, a wing experiences flutter instability, which causes the wing to oscillate. -
FLUID DYNAMICS, Volume IV
http://dx.doi.org/10.1090/psapm/004 PROCEEDINGS OF SYMPOSIA IN APPLIED MATHEMATICS VOLUME IV FLUID DYNAMICS McGRAW-HILL BOOK COMPANY, INC. NEW YORK TORONTO LONDON 1953 FOR THE AMERICAN MATHEMATICAL SOCIETY 80 WATERMAN STREET, PROVIDENCE, RHODE ISLAND PROCEEDINGS OF THE FOURTH SYMPOSIUM IN APPLIED MATHEMATICS OF THE AMERICAN MATHEMATICAL SOCIETY Held at the University of Maryland June 22-23, 1951 COSPONSORED BY THE U.S. NAVAL ORDNANCE LABORATORY M. H. Martin EDITOR EDITORIAL COMMITTEE R. V. Churchill Eric Reissner A. H. Taub Copyright, 1953, by the McGraw-Hill Book Company, Inc. Printed in the United States of America. All rights reserved. This book, or parts thereof, may not be reproduced in any form without permission of the publishers. Library of Congress Catalog Card Number: 52-10326 CONTENTS EDITOR'S PREFACE v Some Aspects of the Statistical Theory of Turbulence 1 BY S. CHANDRASEKHAR A Critical Discussion of Similarity Concepts in Isotropic Turbulence 19 BY C. C. LIN The Nonexistence of Transonic Potential Flow 29 BY ADOLF BUSEMANN On Waves of Finite Amplitude in Ducts (Abstract) 41 BY R. E. MEYER On the Problem of Separation of Supersonic Flow from Curved Profiles .... 47 BY T. Y. THOMAS On the Construction of High-speed Flows 55 BY G. F. CARRIER AND K. T. YEN An Example of Transonic Flow for the Tricomi Gas 61 BY M. H. MARTIN AND W. R. THICKSTUN On Gravity Waves 75 BY A. E. HEINS Hydrodynamics and Thermodynamics 87 BY S. R. DE GROOT Nonuniform Propagation of Plane Shock Waves 101 BY J. M. BURGERS Theory of Propellers 109 BY THEODORE THEODORSEN Numerical Methods in Conformal Mapping 117 BY G. -
Course Syllabus
Course Syllabus Primary Oral Chinese2-1(Course Code 2091199) Course Credits 4 Total Course Hours 64 Lecture Hours 64 Experiment Hours Programming Hours Other Practical Hours Course Instructors: Course Website: 1. Objectives and Learning Outcomes Elementary Spoken Chinese I for non-native speakers of Chinese who wish to develop their communicative skills and cultivate their thinking in Chinese. The course provides various opportunities for students to get involved in different occasions in daily life; thus making it possible for students to master basic vocabulary, special expressions and idioms,and communicate accurately and fluently in Chinese . 2. Course Content Course content Specific learning objectives A preliminary understanding of Pinyin and Chapter 1 – Chapter 2 Pinyin pronunciation, master initials and finals. Chapter 3 Tones, Modified tone, Rhotic accent Master the tones, light tones, Rhotic accent Chapter 4 What’s your name? Learn to introduce oneself briefly Introduce oneself in real communication Chapter 5 Which class are you in? Master interrogative questions and can skillfully use them in daily life. Chapter 6 what time is it now? Asking about time. Able to answer and ask questions fluently using Chapter 7 where is the canteen? location words. Be able to use common shopping expressions to Chapter 8 How much is it in all? answer and ask questions fluently. Comprehensive oral practice Chapter 9 What do you want to do? To communicate by phone Chapter 10 She is sick. Master body parts noun; Learn to ask for leave. Task-based classroom teaching. Master the expression of color. Chapter 11 I like drinking tea. Express what you like.