A Method That Lends Wings
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Gustave Eiffel, a Pioneer of Aerodynamics
Int. J. Engineering Systems Modelling and Simulation, Vol. 5, Nos. 1/2/3, 2013 3 Gustave Eiffel, a pioneer of aerodynamics Bruno Chanetz* Onera, 8 rue des Vertugadins, F-92 190 Meudon, France Fax: +33-1-46-23-51-58 and University Paris-Ouest, LTIE-GTE, EA 4415, 50 rue de Sèvres, F-92410 Ville d’Avray, France Fax: +33-1-40-97-48-73 E-mail: [email protected] E-mail: [email protected] *Corresponding author Martin Peter Laboratoire Aérodynamique Eiffel, 68 rue Boileau, F-75016 Paris E-mail: [email protected] Abstract: At the beginning of the 20th century, Gustave Eiffel contributes with Ludwig Prandtl to establish a new science: aerodynamics. He was going to study the forces to which he was confronted as engineer during his life: gravity and wind. Keywords: Eiffel wind tunnel; diffuser; laminar regime; turbulent regime; transition; drag of the sphere; Eiffel chamber. Reference to this paper should be made as follows: Chanetz, B. and Peter, M. (2013) ‘Gustave Eiffel, a pioneer of aerodynamics’, Int. J. Engineering Systems Modelling and Simulation, Vol. 5, Nos. 1/2/3, pp.3–7. Biographical notes: Bruno Chanetz joins Onera in 1983 as a Research Engineer. He was the Head of Hypersonic Group in 1990, Head of Hypersonic Hyperenthalpic Project in 1997 and Head of Experimental Simulation and Physics of Fluid Unit in 1998, then Deputy Director of the Fundamental and Experimental Aerodynamics Department in 2003. He was a Lecturer in Charge of the course ‘Boundary Layer’ at the Ecole Centrale de Paris from 1996 to 2003, then Associate Professor at the University of Versailles from 2003 to 2009. -
Brief History of the Early Development of Theoretical and Experimental Fluid Dynamics
Brief History of the Early Development of Theoretical and Experimental Fluid Dynamics John D. Anderson Jr. Aeronautics Division, National Air and Space Museum, Smithsonian Institution, Washington, DC, USA 1 INTRODUCTION 1 Introduction 1 2 Early Greek Science: Aristotle and Archimedes 2 As you read these words, there are millions of modern engi- neering devices in operation that depend in part, or in total, 3 DA Vinci’s Fluid Dynamics 2 on the understanding of fluid dynamics – airplanes in flight, 4 The Velocity-Squared Law 3 ships at sea, automobiles on the road, mechanical biomedi- 5 Newton and the Sine-Squared Law 5 cal devices, and so on. In the modern world, we sometimes take these devices for granted. However, it is important to 6 Daniel Bernoulli and the Pressure-Velocity pause for a moment and realize that each of these machines Concept 7 is a miracle in modern engineering fluid dynamics wherein 7 Henri Pitot and the Invention of the Pitot Tube 9 many diverse fundamental laws of nature are harnessed and 8 The High Noon of Eighteenth Century Fluid combined in a useful fashion so as to produce a safe, efficient, Dynamics – Leonhard Euler and the Governing and effective machine. Indeed, the sight of an airplane flying Equations of Inviscid Fluid Motion 10 overhead typifies the laws of aerodynamics in action, and it 9 Inclusion of Friction in Theoretical Fluid is easy to forget that just two centuries ago, these laws were Dynamics: the Works of Navier and Stokes 11 so mysterious, unknown or misunderstood as to preclude a flying machine from even lifting off the ground; let alone 10 Osborne Reynolds: Understanding Turbulent successfully flying through the air. -
RERL Fact Sheet 1, Community Wind Technology
Renewable Energy Research Laboratory, University of Massachusetts at Amherst Wind Power: Wind Technology Today Community Wind Power on the Community Scale Wind Power Fact Sheet # 1 RERL—MTC Community Wind Wind Power Technology for Fact Sheet Series Communities In collaboration with the Mas- sachusetts Technology Col- This introduction to wind power technology is We also recommend a visit to a modern wind laborative’s Renewable Energy meant to help communities begin considering or power installation – it will answer many of your Trust Fund, the Renewable planning wind power. It focuses on commercial initial questions, including size, noise levels, foot- Energy Research Lab (RERL) and medium-scale wind turbine technology avail- print, and local impact. Some possible field trips able in the United States. are listed on the back page. brings you this series of fact sheets about Wind Power on the community scale: Wind Power Today 1. Technology 2. Performance Wind power is a growing industry, and the technol- 3. Impacts & Issues ogy has changed considerably in recent decades. 4. Siting What would a typical commercial-scale* turbine 5. Resource Assessment installed today look like? 6. Wind Data • Design - 3 blades 7. Permitting - Tubular tower The focus of this series of fact • Hub-height - 164 - 262 ft (50 - 80 m) sheets is medium- • Diameter: - 154 - 262 ft (47 - 80 m) and commercial- • Power ratings available in the US: scale wind. - 660 kW - 1.8 MW * Other scales are discussed below. A wind turbine’s height is usually described as the height of the center of the rotor, or hub. Inside this Edition: Technology Size Ranges What do we mean here when we say “community-scale wind power”? Introduction p. -
Active Management of Flap-Edge Trailing Vortices*
4th Flow Control Conference, Seattle, Washington, June 23-26, 2008 Active Management of Flap-Edge Trailing Vortices* David Greenblatt Technion – Israel Institute of Technology, Haifa, Israel Chung-Sheng Yao† NASA Langley Research Center, Hampton VA, USA Stefan Vey,‡ Oliver C. Paschereit¶ Berlin University of Technology, Berlin, Germany Robert Meyer§ German Aerospace Center (DLR), Berlin, Germany The vortex hazard produced by large airliners and increasingly larger airliners entering service, combined with projected rapid increases in the demand for air transportation, is expected to act as a major impediment to increased air traffic capacity. Significant reduction in the vortex hazard is possible, however, by employing active vortex alleviation techniques that reduce the wake severity by dynamically modifying its vortex characteristics, providing that the techniques do not degrade performance or compromise safety and ride quality. With this as background, a series of experiments were performed, initially at NASA Langley Research Center and subsequently at the Berlin University of Technology in collaboration with the German Aerospace Center. The investigations demonstrated the basic mechanism for managing trailing vortices using retrofitted devices that are decoupled from conventional control surfaces. The basic premise for managing vortices advanced here is rooted in the erstwhile forgotten hypothesis of Albert Betz, as extended and verified ingeniously by Coleman duPont Donaldson and his collaborators. Using these devices, vortices may be perturbed at arbitrarily long wavelengths down to wavelengths less than a typical airliner wingspan and the oscillatory loads on the wings, and hence the vehicle, are small. Significant flexibility in the specific device has been demonstrated using local passive and active separation control as well as local circulation control via Gurney flaps. -
Experimenting Close to the Wind
FLASHBACK_Aerodynamics Experimenting Close to the Wind Wind energy is a technology with a future – and with origins that can be traced far back into the past. One of its pioneers was Albert Betz, who was a Director at the Max Planck Institute for Fluid Dynamics in Göttingen from 1947 to 1956. TEXT MICHAEL GLOBIG “When, after the war, our economy was be allowed to flow through without reduc- Inspired by the sophisticated criteria for suffering acutely from the general shortage ing the air speed at all – in which case, aircraft propellers, in the mid-1920s Betz of coal, attention once again turned more once again, no energy would be “tapped.” turned his attention to windmill sails and eagerly to other sources of energy. In addi- discovered that these are subject to the tion to the development of hydropower, it GÖTTINGEN BECOMES THE same laws as propellers: a propeller driven was primarily recommended to make CENTER OF EXISTENCE by an engine creates air pressure, whereas greater use of wind energy. This interest windmills rotate in response to natural air continued even after the coal shortage was It can thus be assumed that, between pressure. Exactly the same aerodynamic overcome.” Albert Betz, who wrote these these two extremes, there must be an area laws apply to both and can be calculated lines, was himself one of the pioneers of in which mechanical energy can be extract- using the same equations. However, wind- wind power. It was he who postulated a ed by slowing the wind down. Upon closer mills with sails that exhibit an exact pro- law, now named after him, that no engi- examination, it becomes apparent that peller shape have a very low starting neer can afford to ignore. -
Ludwig Prandtl and Boundary Layers in Fluid Flow How a Small Viscosity Can Cause Large Effects
GENERAL I ARTICLE Ludwig Prandtl and Boundary Layers in Fluid Flow How a Small Viscosity can Cause large Effects Jaywant H Arakeri and P N Shankar In 1904, Prandtl proposed the concept of bound ary layers that revolutionised the study of fluid mechanics. In this article we present the basic ideas of boundary layers and boundary-layer sep aration, a phenomenon that distinguishes stream lined from bluff bodies. Jaywant Arakeri is in the Mechanical Engineering A Long-Standing Paradox Department and in the Centre for Product It is a matter of common experience that when we stand Development and in a breeze or wade in water we feel a force which is Manufacture at the Indian called the drag force. We now know that the drag is Institute of Science, caused by fluid friction or viscosity. However, for long it Bangalore. His research is was believed that the viscosity shouldn't enter the pic mainly in instability and turbulence in fluid motion. ture at all since it was so small in value for both water He is also interested in and air. Assuming no viscosity, the finest mathematical issues related to environ physicists of the 19th century constructed a large body ment and development. of elegant results which predicted that the drag on a body in steady flow would be zero. This discrepancy between ideal fluid theory or hydrodynamics and com mon experience was known as 'd' Alembert's paradox' The paradox was only resolved in a revolutionary 1904 paper by L Prandtl who showed that viscous effects, no matter how'small the viscosity, can never be neglected. -
Chapter on Prandtl
2 Prandtl and the Gottingen¨ school Eberhard Bodenschatz and Michael Eckert 2.1 Introduction In the early decades of the 20th century Gottingen¨ was the center for mathemat- ics. The foundations were laid by Carl Friedrich Gauss (1777–1855) who from 1808 was head of the observatory and professor for astronomy at the Georg August University (founded in 1737). At the turn of the 20th century, the well- known mathematician Felix Klein (1849–1925), who joined the University in 1886, established a research center and brought leading scientists to Gottingen.¨ In 1895 David Hilbert (1862–1943) became Chair of Mathematics and in 1902 Hermann Minkowski (1864–1909) joined the mathematics department. At that time, pure and applied mathematics pursued diverging paths, and mathemati- cians at Technical Universities were met with distrust from their engineering colleagues with regard to their ability to satisfy their practical needs (Hensel, 1989). Klein was particularly eager to demonstrate the power of mathematics in applied fields (Prandtl, 1926b; Manegold, 1970). In 1905 he established an Institute for Applied Mathematics and Mechanics in Gottingen¨ by bringing the young Ludwig Prandtl (1875–1953) and the more senior Carl Runge (1856– 1927), both from the nearby Hanover. A picture of Prandtl at his water tunnel around 1935 is shown in Figure 2.1. Prandtl had studied mechanical engineering at the Technische Hochschule (TH, Technical University) in Munich in the late 1890s. In his studies he was deeply influenced by August Foppl¨ (1854–1924), whose textbooks on tech- nical mechanics became legendary. After finishing his studies as mechanical engineer in 1898, Prandtl became Foppl’s¨ assistant and remained closely re- lated to him throughout his life, intellectually by his devotion to technical mechanics and privately as Foppl’s¨ son-in-law (Vogel-Prandtl, 1993). -
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Memorial Tributes: Volume 3 ADOLF BUSEMANN 62 Copyright National Academy of Sciences. All rights reserved. Memorial Tributes: Volume 3 ADOLF BUSEMANN 63 Adolf Busemann 1901–1986 By Robert T. Jones Adolf Busemann, an eminent scientist and world leader in supersonic aerodynamics who was elected to the National Academy of Engineering in 1970, died in Boulder, Colorado, on November 3, 1986, at the age of eighty-five. At the time of his death, Dr. Busemann was a retired professor of aeronautics and space science at the University of Colorado in Boulder. Busemann belonged to the famous German school of aerodynamicists led by Ludwig Prandtl, a group that included Theodore von Karman, Max M. Munk, and Jakob Ackeret. Busemann was the first, however, to propose the use of swept wings to overcome the problems of transonic and supersonic flight and the first to propose a drag-free system of wings subsequently known as the Busemann Biplane. His ''Schock Polar,'' a construction he described as a "baby hedgehog," has simplified the calculations of aerodynamicists for decades. Adolf Busemann was born in Luebeck, Germany, on April 20, 1901. He attended the Carolo Wilhelmina Technical University in Braunschweig and received his Ph.D. in engineering there in 1924. In 1930 he was accorded the status of professor (Venia Legendi) at Georgia Augusta University in Goettingen. In 1925 the Max-Planck Institute appointed him to the position of aeronautical research scientist. He subsequently Copyright National Academy of Sciences. All rights reserved. Memorial Tributes: Volume 3 ADOLF BUSEMANN 64 held several positions in the German scientific community, and during the war years, directed research at the Braunschweig Laboratory. -
1903 Wright Flyer I National Air & Space Museum
NASANASA VisionVision && MissionMission NASA vision is: • Innovation • Inspiration • Discovery The NASA mission is: • Technology innovation • Inspiration for the next generation • And discovery in our universe as only NASA can TheThe WrightWright BrothersBrothers andand thethe FutureFuture ofof Bio-InspiredBio-Inspired FlightFlight 1899 through to the Future… Al Bowers NASA Dryden Flight Research Center North Carolina State University Raleigh, NC 28 November 2007 Background:Background: TheThe TimesTimes TranscontinentalTranscontinental RailroadRailroad…… - the great engineering achievement of the time - understanding of “two-track” vehicle systems (buggys, carts, & trains) - completed on 10 May 1869 (Wilbur was two years old) Background:Background: ProgenitorsProgenitors • Otto Lilienthal - experiments from 1891 to 1896 • Samuel P Langley - experiments from 1891-1903 • Octave Chanute - experiments from 1896-1903 OttoOtto LilienthalLilienthal • Glider experiments 1891 - 1896 DrDr SamuelSamuel PierpontPierpont LangleyLangley • Aerodrome experiments 1887-1903 OctaveOctave ChanuteChanute • Gliding experiments 1896 to 1903 WilburWilbur andand OrvilleOrville 16 Apr 1867 – 30 May 1912 19 Aug 1871 – 30 Jan 1948 WrightWright BrothersBrothers TimelineTimeline • 1878 The Wrights receive a gift of a toy helicopter • 1895 The Wrights begin to manufacture their own bicycles • 1896 The Wrights take an interest in the "flying problem" • 1899 Wilbur devises a revolutionary control system, builds a kite to test it; also writes the Smithsonian. • 1900 The -
On the Minimum Induced Drag of Wings
On the Minimum Induced Drag of Wings Albion H. Bowers NASA Dryden Flight Research Center AIAA/SFTE AV Chapters Lancaster, CA 16 August, 2007 Introduction λ The History of Spanload Development of the optimum spanload Winglets and their implications λ Horten Sailplanes λ Flight Mechanics & Adverse yaw λ Concluding Remarks History λ Bird Flight as the Model for Flight λ Vortex Model of Lifting Surfaces λ Optimization of Spanload Prandtl Prandtl/Horten/Jones Klein/Viswanathan λ Winglets - Whitcomb Birds Bird Flight as a Model or “Why don’t birds have vertical tails?” λ Propulsion Flapping motion to produce thrust Wings also provide lift Dynamic lift - birds use this all the time (easy for them, hard for us) λ Stability and Control Still not understood in literature Lack of vertical surfaces λ Birds as an Integrated System Structure Propulsion Lift (performance) Stability and control Dynamic Lift Early Mechanical Flight λ Otto & Gustav Lilienthal (1891-1896) λ Octave Chanute (1896-1903) λ Samuel P Langley (1896-1903) λ Wilbur & Orville Wright (1899-1905) Otto Lilienthal λ Glider experiments 1891 - 1896 Dr Samuel Pierpont Langley λ Aerodrome experiments 1887-1903 Octave Chanute λ Gliding experiments 1896 to 1903 Wilbur & Orville Wright λ Flying experiments 1899 to 1905 Spanload Development λ Ludwig Prandtl Development of the boundary layer concept (1903) Developed the “lifting line” theory Developed the concept of induced drag Calculated the spanload for minimum induced drag (1908?) Published in open literature (1920) λ Albert Betz Published -
Schnellflug- Und Pfeilflügeltechnik
Der weitere Rundgang in der Halle 2 - die Schnellflugausstellung und die Geschichte der aerodynamischen Pfeilflügeltechnik mit der durch sie veränderten Welt Bevor wir Sie weiter durch unsere Ausstellung führen, wollen wir Sie ein wenig über die Hintergründe unserer Arbeit vertraut machen. Wir benötigen dafür Fachwissen mit breitem Hintergrund, und das müssen wir zusammen- tragen. Im Lauf der letzten 25 Jahre ist das eine stattliche Menge geworden und wird in unserem Archiv in einem Nebengebäude bearbeitet und verwaltet. Selbstverständlich müssen schon Grundkenntnisse durch eine längere Beschäftigung mit diesem komplexen Thema vorhanden sein, seien es technische, historische oder noch andere Zugänge. Unser Archiv: Oben links die Büchersammlung, rechts ebenso mit einem Teil der Flugzeug- Typensammlung, unten die Buchstaben A - D der Typensammlung in den A4-Ordnern. Doch kann man sich auch als Fachfremder gut darin einarbeiten, wenn man "zur Stange" hält. Wir alle sind als ehrenamtliche Mitarbeiter im Museumsteam keine studierten Museums- pädagogen oder sonstige Fachwissenschaftler, sondern Menschen aus allen möglichen Berufen, Handwerker und Juristen, Verwaltungsleute und Mediziner. Uns eint die Liebe zur Fliegerei, deren Technik und der Wille zur historischen Einordnung. Und ordentlich mit solchen Themen umzugehen, haben wir in anderen Berufen gelernt. Im Archivgebäude haben wir mehrere Räume, in denen einmal so um 4 - 5 tausend Bücher, diverse Luftfahrtzeitschriften und andere Periodika versammelt sind. Dazu kommt eine ausgedehnte Flugzeugtypensammlung, die sich aus Veröffentlichungen einheimischer und auswärtiger Luftfahrtzeitschriften über die letzen 60 - 70 Jahre speist, mit Motor-, Segel- und UL-Flugzeugen sowie Hubschraubern. Das sind noch einmal gute 800 A-4 Bände, Die verschiedenen Typen sind nach Herstellern alphabetisch sortiert. Dieses Archiv dürfen Sie nach tel. -
Prandtl's Flow Visualization Film C1 Revisited
13th International Symposium on Particle Image Velocimetry – ISPIV 2019 Munich, Germany, July 22-24, 2019 Prandtl’s flow visualization film C1 revisited Christian Willert1∗, Mario Schulze2, Sarine Waltenspul¨ 2, Daniel Schanz3, Jurgen¨ Kompenhans3 1 German Aerospace Center (DLR), Institute of Propulsion Technology, Koln,¨ Germany 2 Zurich University of the Arts, Zurich, Switzerland 3 German Aerospace Center (DLR), Institute of Aerodynamics and Flow Technology, Gottingen,¨ Germany ∗ [email protected] Abstract We would like to report on the techniques used around 1930 for the creation of a film consisting of se- quences visualizing various forms of flow separation produced by L. Prandtl and his colleagues O. Tietjens and W. Muller¨ in open-surface water channels. After first experiments with cinematography in the 1910s, Prandtl began to produce flow visualisation films in the 1920s, in order to better capture the dynamics of the unsteady flow phenomena. However, due to the short exposure times provided by the film camera the particles appeared as dots rather than the anticipated streaks, which were desired as representations of the streamlines. Therefore Prandtl and his colleagues first decided to work with a modified camera to provide longer exposure time and consequently streaked images. At this point, the real potential of animated film, for instance for the demonstration of flow separation, was realized and resulted in a flow visualization film, originally named “The Production of Vortices by Bodies Travelling in Water”, that Prandtl showed 1927 in London and while travelling the globe from 1929 to 1930. The sequences of this film were found to be highly instructive from an educational point of view such that the film, now named C1, was made available in 1936 through the Reich Office for Teaching Films and in the 1950s by the Institute of Scientific Film.