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Dissertations / Theses on the topic 'NACA 0018'

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Published: 4 June 2021

Last updated: 26 July 2025

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1

Oliveira, Thiago Fernandes. "Estudo experimental do estol dinâmico em um aerofólio naca 0018." reponame:Repositório Institucional da UnB, 2011. http://repositorio.unb.br/handle/10482/9388.

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Dissertação (mestrado)—Universidade de Brasília, Departamento de Engenharia Mecânica, 2011.<br>Submitted by Shayane Marques Zica (marquacizh@uol.com.br) on 2011-09-13T19:13:31Z No. of bitstreams: 1 2011_ThiagoFernandesOliveira.pdf: 4245386 bytes, checksum: 1a6804b340c8e4f82fe6c1591dffe1e9 (MD5)<br>Approved for entry into archive by LUCIANA SETUBAL MARQUES DA SILVA(lucianasetubal@bce.unb.br) on 2011-10-04T16:16:42Z (GMT) No. of bitstreams: 1 2011_ThiagoFernandesOliveira.pdf: 4245386 bytes, checksum: 1a6804b340c8e4f82fe6c1591dffe1e9 (MD5)<br>Made available in DSpace on 2011-10-04T16:16:42Z (

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2

Bonavita, Gianluca. "Ottimizzazione costruttiva e di montaggio di un aerogeneratore ad asse verticale privo di fondazione." Master's thesis, Alma Mater Studiorum - Università di Bologna, 2012. http://amslaurea.unibo.it/3666/.

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3

Yu, Hongtao. "A Validation Study of SC/Tetra CFD Code." Wright State University / OhioLINK, 2014. http://rave.ohiolink.edu/etdc/view?acc_num=wright1399896316.

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4

Islam, Md Monirul. "Nonlinear normal force indicial responses for a 2-D NACA 0015 airfoil." Ohio : Ohio University, 1991. http://www.ohiolink.edu/etd/view.cgi?ohiou1183730957.

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5

Fang, Kuan-Chieh. "Nonlinear aerodynamic responses in tow tank study for a two dimensional NACA 0015 airfoil." Ohio : Ohio University, 1992. http://www.ohiolink.edu/etd/view.cgi?ohiou1172265691.

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6

Li, Sihao. "Effect of aeroelasticity in tow tank strain gauge measurements on a NACA 0015 airfoil." Ohio : Ohio University, 1993. http://www.ohiolink.edu/etd/view.cgi?ohiou1175713922.

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7

Fernie, Robert Mark. "Low frequency shock motion on a NACA 0012 aerofoil." Thesis, University of Cambridge, 2005. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.614936.

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8

Jensen, Christopher Douglas. "Global Pressure and Temperature Surface Measurements on a NACA 0012 Airfoil in Oscillatory Compressible Flow at Low Reduced Frequencies." The Ohio State University, 2012. http://rave.ohiolink.edu/etdc/view?acc_num=osu1331075431.

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9

Digavalli, Sasi K. (Sasi Kumar). "Dynamic stall of a NACA 0012 airfoil in laminar flow." Thesis, Massachusetts Institute of Technology, 1993. http://hdl.handle.net/1721.1/12206.

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10

Castañeda, Vergara David Armando. "Active Control of Flow over an Oscillating NACA 0012 Airfoil." The Ohio State University, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=osu1587420875168203.

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11

Heyd, Darrick Vaughn. "Photodissociation of methyl bromide adsorbed on LiF(001), NaCl(001), and MgO(001)." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 1997. http://www.collectionscanada.ca/obj/s4/f2/dsk2/tape16/PQDD_0001/NQ27950.pdf.

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12

Sahoo, Dipankar. "Experimental analysis of the vorticity and turbulent flow dynamics of a pitching airfoil at realistic flight (helicopter) conditions." Diss., Texas A&M University, 2008. http://hdl.handle.net/1969.1/85893.

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Improved basic understanding, predictability, and controllability of vortex-dominated and unsteady aerodynamic flows are important in enhancement of the performance of next generation helicopters. The primary objective of this research project was improved understanding of the fundamental vorticity and turbulent flow physics for a dynamically stalling airfoil at realistic helicopter flight conditions. An experimental program was performed on a large-scale (C = 0.45 m) dynamically pitching NACA 0012 wing operating in the Texas A&M University large-scale wind tunnel. High-resolution particle ima

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13

Nowak, Lisa M. "Computational investigations of a NACA 0012 airfoil in low Reynolds number flows." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1992. http://edocs.nps.edu/npspubs/scholarly/theses/1992/Sep/92Sep_Nowak.pdf.

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Thesis (Degree in Aeronautical and Astronautical Engineer)--Naval Postgraduate School, Sept. 1992.<br>Thesis advisor(s): M.F. Platzer and M. Chandrasekhara. "September 1992." Includes bibliographical references. Also available online.

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14

Debien, Antoine. "Étude électromécanique et optimisation d'actionneurs plasmas à décharge à barrièrediélectrique – Application au contrôle de décollement sur un profil d'aile de type NACA0015." Thesis, Poitiers, 2013. http://www.theses.fr/2013POIT2253/document.

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Cette thèse est effectuée dans le cadre du projet Européen "PlasmAero" dont le but est de développer et d'étudier des actionneurs plasmas, et de démontrer leur capacité à contrôler des écoulements aérodynamiques. L'actionneur plasma à Décharge à Barrière Diélectrique (DBD) de surface est un moyen innovant pour contrôler un écoulement en utilisant le vent électrique induit par la force électrohydrodynamique (EHD) générée au sein du gaz ionisé. Une première partie est dédiée à l'étude des actionneurs plasmas. L'influence de la géométrie de l'électrode active d'une DBD est précisée par des mesure

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15

Clifford, Christopher J. "An Investigation of Physics and Control of Flow Passing a NACA 0015 in Fully-Reversed Condition." The Ohio State University, 2015. http://rave.ohiolink.edu/etdc/view?acc_num=osu1440156651.

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16

Singhal, Achal Sudhir. "Unsteady Flow Separation Control over a NACA 0015 using NS-DBD Plasma Actuators." The Ohio State University, 2017. http://rave.ohiolink.edu/etdc/view?acc_num=osu148217512319911.

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17

Sinha, Roy Arijit. "Analysis and control of boundary layer transition on a NACA 0008 wing profile." Thesis, KTH, Mekanik, 2018. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-239931.

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The main aim of this thesis was to understand the mechanism behind the classical transition scenario inside the boundary layer over an airfoil and eventually attempting to control this transition utilizing passive devices for transition delay. The initial objective of analyzing the transition phenomenon based on TS wave disturbance growth was conducted at 90 Hz using LDV and CTA measurement techniques at two different angles of attack. This was combined with the studies performed on two other frequencies of 100 and 110 Hz, in order to witness its impact on the neutral stability curve behavior.

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18

Audier, Pierre. "Etude d'une décharge à barrière diélectrique surfacique. Application au contrôle d'écoulement autour d'un profil d'aile de type NACA 0012." Phd thesis, Université d'Orléans, 2012. http://tel.archives-ouvertes.fr/tel-00843633.

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Dans un contexte de croissance du trafic aérien et dans le but de réduire la consommation de carburant ainsi que les émissions de polluants dans l'atmosphère, l'avion de demain se doit d'être plus respectueux de l'environnement. Dans un objectif d'optimisation de ses performances aérodynamiques,d'importantes activités de recherche sont menées dans le monde pour étudier de nouveaux dispositifs de contrôle actif des écoulements en temps réel. Depuis une dizaine d'années, l'utilisation de la décharge à barrière diélectrique surfacique comme actionneur plasma pour le contrôle d'écoulements suscite

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19

Beck, Paulo Arthur. "Análise metodológica de simulações de escoamentos turbulentos sobre seções de perfis aerodinâmicos." reponame:Biblioteca Digital de Teses e Dissertações da UFRGS, 2010. http://hdl.handle.net/10183/28925.

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Este trabalho apresenta o resultado da aplicação do Método dos Volumes Finitos, adotado pelo software comercial Star-CCM+ na simulação para o regime permanente de escoamentos turbulentos incompressíveis e compressíveis sobre seções de aerofólios. Para o caso incompressível modelam-se seções do aerofólio NACA 0012 com ângulo de ataque zero. Para o caso compressível, uma seção do aerofólio supercrítico OAT15A em pequeno ângulo de ataque é modelada. Os domínios computacionais são discretizados por malhas não estruturadas de células poliédricas ou por malhas estruturadas de geração hiperbólica par

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20

Sullivan, Taylor D. "REDUCED ORDER MODELING OF FLOW OVER A NACA 0015 AIRFOIL FOR FUTURE CONTROL APPLICATION." Miami University / OhioLINK, 2014. http://rave.ohiolink.edu/etdc/view?acc_num=miami1407295741.

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21

Song, Longfei. "Leading-edge flow separation control over a NACA 0012 aerofoil with DBD plasma actuators." Thesis, University of Nottingham, 2018. http://eprints.nottingham.ac.uk/49841/.

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An experimental investigation has been conducted in a low-speed wind tunnel at the University of Nottingham to study the flow separation control capability of a wall-normal plasma jet by DBD plasma actuator over a NACA 0012 aerofoil. As an active flow separation control technique, DBD plasma actuators could be applied when required to manipulate a flow. They are surface-mounted and require no moving parts, ducts, holes or cavities, so no profile drag penalty will be caused. Moreover, they are fast responding since they are purely electrical devices and could be operated at a higher frequency r

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22

Hu, Wei. "Monte Carlo simulations of the CO¦2/NaCI(001) and CH¦3Br/LiF(001) systems." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 1997. http://www.collectionscanada.ca/obj/s4/f2/dsk2/ftp04/mq25989.pdf.

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23

Métivier, Vincent. "Étude des oscillations auto-excitées d'un profil d'aile NACA 0012 à des nombres de Reynolds transitionnels." Thesis, Université Laval, 2012. http://www.theses.ulaval.ca/2012/28696/28696.pdf.

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24

Tsiachris, Fotios K. "Retreating blade stall control on a NACA 0015 aerofoil by means of a trailing edge flap." Thesis, University of Glasgow, 2005. http://theses.gla.ac.uk/5109/.

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Trailing edge flaps may provide a mechanism for alleviating retreating blade stall. In the present investigation numerical simulations were conducted involving a NACA 0015 aerofoil section fitted with a plain trailing edge (TE) flap. All simulations were conducted using DIVEX, a tool being developed at the University of Glasgow, Department of Aerospace Engineering. In summary, the code uses a surface shedding discrete vortex method (DVM) for the simulation of 2-D incompressible flows around pitching aerofoils. The aero-foil is oscillating in pitch about its quarter chord axis and the clap unde

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25

L'Esperance, Alan M. "Experimental Study of Delay of Separation on a NACA 0015 Wing Model Using Synthetic Jet Actuators." DigitalCommons@CalPoly, 2014. https://digitalcommons.calpoly.edu/theses/1287.

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An experimental study has been conducted in the Cal Poly ME 0.61 m x 0.61 m (2 ft x 2 ft) subsonic wind tunnel of the effect of a piezoelectric synthetic jet actuator at 10% chord on a NACA 0015 finite wing up to α = 20° at ReC = 100,000. It was observed that the actuation is able to delay the separation over the NACA 0015 finite wing model up to α = 20°. For all the Cμ values tested, the synthetic jet excitation is effective at F+ = 1, 2.8, and 13.9 at α = 16°, but only at F+ = 13.9 at α = 20°. At α = 16°, the Cp suction peak under the synthetic jet excitation at F+ = 1, 2.8, and 13.9 all gra

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26

Siauw, Wei Long. "Transient process of separation and attachment over a NACA 0015 airfoil controlled by fluidic vortex generators." Poitiers, 2008. http://www.theses.fr/2008POIT2313.

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Ce travail expérimental est consacré à l’étude du décollement et du recollement transitoire sur profil NACA 0015 contrôlé par des Générateurs de Vortex Fluidique (FVG). Des essais sont effectués à un nombre de Reynolds de 1 million, et à une incidence de 11o. L’écoulement sans contrôle est caractérisé par une zone décollée qui commence à xA-c=0,7 à partir du bord d'attaque (soit 30% de la corde) avec un minimum de vibrations. Pour effectuer le contrôle de l’écoulement, 44 FVG sont installés à xA-c=0,3. Les effets de la FVG sont caractérisés par une augmentation de 16% du coefficient de portanc

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27

Lundberg, Marcus. "Aerodynamics of Insect Flight : Effects of wind gusts on a rigid flapping NACA 0012 airfoil at Re = 3000." Thesis, KTH, Mekanik, 2015. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-167123.

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Insects and small flyers operate at Reynolds numbers ranging from approximately 10-105 , where viscous forces are important. Due to their small size and weight, they are sensitive to small changes in the free stream during flight, such as wind gusts. First, the aerodynamics of flapping flight is briey explained. Then the lift, drag and power usage for a flapping NACA 0012 airfoil is simulated in ANSYS Fluent for different oncoming wind directions. The aim of the report is to understand how the pitching amplitude, the apping frequency and the plunging amplitude can be adjusted to compensate for

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28

Goffert, Bruno. "Análise numérica e experimental de escoamento transônico sobre o aerofólio NACA 0012 no túnel transônico piloto do IAE." Instituto Tecnológico de Aeronáutica, 2012. http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2140.

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Experimentos em escoamentos transônicos sobre aerofólios em túneis de vento podem apresentar reflexões de ondas de choque, entupimento aerodinâmico e alteração das linhas de corrente devido à presença das paredes da seção de testes. Para inibir estes fenômenos físicos, projetistas desenvolveram seções de testes com paredes perfuradas ou fendidas. O objetivo deste trabalho é analisar numericamente e experimentalmente escoamento transônico sobre o aerofólio NACA 0012 no Túnel Transônico Piloto (TTP) do Instituto de Aeronáutica e Espaço (IAE). As análises foram realizadas com número de Mach 0,6 a

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29

Mikat, Jürgen E. R. "Optische und schwingungsspektroskopische Hochdruckuntersuchungen von Ladungsträgereigenschaften in herkömmlich und nach der Template-Methode synthetisierten leitfähigen Polypyrrolschichten." [S.l. : s.n.], 2001. http://pub.ub.uni-potsdam.de/2001/0013/mikat.pdf.

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30

Hustedt, Michael. "Zur Adsorption von CO2 auf NaCl(001)- und KCl(001)-Einkristallspaltflächen höchstauflösende Polarisations-Fouriertransform-Infrarot-Spektroskopie, Diodenlaserspektroskopie, Beugung langsamer Elektronen und Spektrensimulationen /." [S.l. : s.n.], 1999. http://deposit.ddb.de/cgi-bin/dokserv?idn=955904102.

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31

Mish, Patrick F. "Mean Loading and Turbulence Scale Effects on the Surface Pressure Fluctuations Occurring on a NACA 0015 Airfoil Immersed in Grid Generated Turbulence." Thesis, Virginia Tech, 2001. http://hdl.handle.net/10919/33751.

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Detailed surface pressure measurements have been made on a NACA 0015 immersed in two grid generated homogenous flows at Re = 1.17 x 10^6 for a = 0Â°, 4Â°, 8Â°, 12Â°, 16Â°, and 20Â°. The goal of this measurement was to reveal and highlight mean loading and turbulence scale effects on surface pressure fluctuations resulting from turbulence/airfoil interaction. Also, measurements are compared with the theory of Amiet (1976a,b). The surface pressure response shows a dependance on angle of attack, the nature of which is related to the relative chord/turbulence scale. The dependance on turbulenc

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32

Van, Dyken Robert D. "Experimental and computational analysis of separation bubble behavior for compressible, steady and oscillatory flows over a NACA 0012 airfoil at M=0.3 and a reynolds number of 540,000." Thesis, Monterey, California. Naval Postgraduate School, 1997. http://hdl.handle.net/10945/8365.

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Approved for public release; distribution is unlimited<br>In this thesis, the separation bubble behavior and its effect on the steady and dynamic stall characteristics of a thin airfoil in a compressible flow at a transitional Reynolds number was studied. For such flows, laminar separation occurs near the airfoil leading edge, but turbulent reattachment occurs within a short distance downstream, forming a separation bubble in the underlying region. Two experimental techniques, point diffraction interferometry (PDI) and laser doppler velocimetry (LDV), were used to acquire detailed flowfield in

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33

Gertz, Roman Johannes [Verfasser]. "Effekt unterschiedlicher Conditioning-Strategien auf myokardiale Funktion und Prognose nach ST-Strecken-Hebungs-Myokardinfarkt / Roman Johannes Gertz." Göttingen : Niedersächsische Staats- und Universitätsbibliothek Göttingen, 2021. http://nbn-resolving.de/urn:nbn:de:gbv:7-21.11130/00-1735-0000-0008-5901-3-1.

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34

Benda, Stefan [Verfasser]. "Einfluss von salzreicher Ernährung auf die hyperperfundierte Niere nach Uninephrektomie bei hereditären Nierenerkrankungen wie dem Alport-Syndrom im Mausmodell / Stefan Benda." Göttingen : Niedersächsische Staats- und Universitätsbibliothek Göttingen, 2021. http://nbn-resolving.de/urn:nbn:de:gbv:7-21.11130/00-1735-0000-0008-58DD-D-4.

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35

Traeger, Franziska. "Streuexperimente mit Wasserstoff- und Heliumstrahlen zur Untersuchung der Wechselwirkung von H2, N2 und C2H2 mit den (001)-Oberflächen von LiF, NaCl, KCl und MgO." [S.l. : s.n.], 2001. http://deposit.ddb.de/cgi-bin/dokserv?idn=963022342.

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36

Oelze, Christiane Verfasser], Hermann [Akademischer Betreuer] [Staats, Dirk [Akademischer Betreuer] Wedekind, and Patricia [Akademischer Betreuer] Virsik-köpp. "Bestimmung Zentraler Beziehungskonfliktthemen (nach Luborsky) bei Patienten mit generalisierter Angststörung : Vergleich der Qualität unterschiedlicher Auswertungsmethoden und Therapieverfahren / Christiane Oelze. Gutachter: Hermann Staats ; Dirk Wedekind ; Patricia Virsik-Köpp. Betreuer: Hermann Staats." Göttingen : Niedersächsische Staats- und Universitätsbibliothek Göttingen, 2013. http://nbn-resolving.de/urn:nbn:de:gbv:7-11858/00-1735-0000-0019-859F-4-4.

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37

Ramalho, Diogo Almeida. "Desempenho das ferramentas cfMesh e snappyHexMesh para geração da malha em torno de perfis alares." Master's thesis, 2015. http://hdl.handle.net/10316/38984.

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Dissertação de Mestrado Integrado em Engenharia Mecânica apresentada à Faculdade de Ciências e Tecnologia da Universidade de Coimbra<br>O objetivo do trabalho apresentado é o estudo da eficiência do gerador de malha cfMesh na criação da malha em torno de um perfil alar, NACA 0018. Os geradores de malha são, tal como o nome indica, responsáveis pela geração da malha usada nos estudos de dinâmica dos fluidos computacional (CFD). Este gerador, ou algoritmo, é relativamente recente mas que segundo alguns estudos, este apresenta resultados interessantes na forma como gera a malha em torno de um per

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Boutilier, Michael Stephen Hatcher. "Experimental Investigation of Transition over a NACA 0018 Airfoil at a Low Reynolds Number." Thesis, 2011. http://hdl.handle.net/10012/6044.

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Shear layer development over a NACA 0018 airfoil at a chord Reynolds number of 100,000 was investigated experimentally. The effects of experimental setup and analysis tools on the results were also examined. The sensitivity of linear stability predictions for measured separated shear layer velocity profiles to both the analysis approach and experimental data scatter was evaluated. Analysis approaches that are relatively insensitive to experimental data scatter were identified. Stability predictions were shown to be more sensitive to the analysis approach than to experimental data scatter, wit

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Bernardo, André Rodrigues. "Estudo das características aerodinâmicas de perfis alares." Master's thesis, 2017. http://hdl.handle.net/10316/83064.

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Dissertação de Mestrado Integrado em Engenharia Mecânica apresentada à Faculdade de Ciências e Tecnologia<br>Esta dissertação de mestrado tem como objectivo estudar as forças que actuam sobre asas com diferentes alongamentos, quando sujeitas a um escoamento subsónico. As asas estudadas têm um perfil simétrico NACA 0012. Este estudo foi realizado no Laboratório de Mecânica dos Fluidos do Departamento de Engenharia Mecânica.Foi estudada a variação da intensidade e direcção das forças e momentos aplicados na asa, e dos respectivos coeficientes aerodinâmicos, com a variação do ângulo de ataque, do

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Pruski, Brandon. "Leading Edge Flow Structure of a Dynamically Pitching NACA 0012 Airfoil." Thesis, 2012. http://hdl.handle.net/1969.1/148372.

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The leading edge flow structure of the NACA 0012 airfoil is experimentally investigated under dynamic stall conditions (M = 0.1; α = 16.7◦, 22.4◦; Rec = 1× 10^6) using planar particle image velocimetry. The airfoil was dynamically pitched about the 1/4 chord at a reduced frequency, k = 0.1. As expected, on the upstroke the flow remains attached in the leading edge region above the static stall angle, whereas during downstroke, the flow remains separated below the static stall angle. A phase averaging procedure involving triple velocity decomposition in combination with the Hilbert transform en

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41

Hu, Wei. "Monte Carlo simulations of the CO₂/NaCl(001) and CH₃Br/LiF(001) systems." Thesis, 1997. http://spectrum.library.concordia.ca/188/1/MQ25989.pdf.

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Metropolis Monte Carlo simulations were used to examine the stable structures, phase coexistence and mechanism of nucleation and growth of films of CO$\sb2$ molecules adsorbed on the (001) surface of NaCl. This was done for submonolayer, monolayer, and multilayer coverages. The results show that the monolayer has two stable structures, a (2 x 1) herringbone structure and a (1 x 1) structure while the bilayer system has three stable structures: the (2 x 1), the (1 x 1) and the c(2 x 2). The trilayer system adopts a c(2 x 2) structure owing to the instability of the (2 x 1) structure. Multilaye

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42

Hung, Wei-Chia, and 洪偉家. "The Effects of Surface Roughness on the Characteristics of Surface Pressure of NACA 0015 Airfoil." Thesis, 2005. http://ndltd.ncl.edu.tw/handle/68260099098319045875.

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碩士<br>國立中興大學<br>機械工程學系<br>93<br>The present study was intended to investigate the surface pressure of NACA 0015 airfoil at upper and lower surface due to the sandblast roughness. The experiment was proceeded in an low-speed and open-type wind tunnel. The dynamic behavior of surface pressure of NACA 0015 airfoil was analyzed at various angle of attack, Reynolds number, number of sandblast, and width of sandblast. The freestream velocity was operated at 5~20 m/s and the corresponding Reynolds number at 3.8×104~1.5×105 which based on the chord of the wing. The purpose of this study was intended t

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43

Knabke, Diana. "Sportfähigkeit nach vorderer Kreuzbandplastik." Doctoral thesis, 2013. http://hdl.handle.net/11858/00-1735-0000-001D-AFA5-B.

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Die Ruptur des vorderen Kreuzbandes ist die häufigste Verletzung des Kniegelenkes. Ziel dieser prospektiven klinischen Studie ist es, Kriterien wie Operationsmethode- und zeitpunkt, subjektive Patientenzufriedenheit, Alltagsfähigkeit und betriebene Sportarten nach der Kreuzbandersatzplastik in verschiedenen Abhängigkeiten voneinander zu diskutieren. Um eine möglichst allgemeingültige Aussage treffen zu können, umfasst die Studie ein nicht-selektives Patientenkollektiv, das Männer und Frauen, Sportler und Nicht-Sportler, Schüler, Studenten und Berufstätige beinhaltet. Außerdem handelt es sich u

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Sallabi, Abdulwahab K. "Computer simulations of the structure, stability and phase transitions of diatomic molecules physisorbed on ionic surfaces : the CO/MgO(001), N2/MgO(001) and N2/NaCl(001) systems." Thesis, 2002. http://spectrum.library.concordia.ca/1715/1/NQ68200.pdf.

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Metropolis Monte Carlo simulations, using semiempirical potentials, are performed to study the structures, stability, and phase transitions of layers of CO and N 2 molecules physisorbed on the MgO(100) surface as well as a monolayer of N 2 physisorbed on NaCl(001) surface. In agreement with experiments [35-37], our simulations show that the c (4 x 2) structure of CO on the MgO(001) surface is the most stable structure below 41 K. The unit cell contains three CO molecules; two bridging molecules tilted in opposite directions by the same polar angle of 31 ̕with respect to the surface normal and

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45

Otten, Birte. "Zeit/Geschichte: Amerikanische Alternate Histories nach 9/11." Doctoral thesis, 2013. http://hdl.handle.net/11858/00-1735-0000-0028-8697-8.

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Zeit/Geschichte: Amerikanische Alternate Histories nach 9/11 untersucht die Entwicklung kontrafaktischer Geschichtstexte, sogenannter alternate histories, vor dem Hintergrund des öffentlichen Diskurses in den USA nach dem 11. September 2001. Dabei konzentriert sich die Studie auf die formalen und generischen Eigenschaften neuerer „Mainstream-alternate histories“ seit den Terroranschlägen. Obwohl keiner der drei untersuchten Texte – Philip Roths The Plot Against America, Michael Chabons The Yiddish Policemen's Union sowie Quentin Tarantinos Inglourious Basterds – von den 9/11-Anschlägen handelt

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46

Knust, Elisabeth. "Histopathologische Veränderungen im zentralen Nervensystem nach peripherer Stammzelltransplantation." Doctoral thesis, 2016. http://hdl.handle.net/11858/00-1735-0000-0028-86EC-A.

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Oelze, Christiane. "Bestimmung Zentraler Beziehungskonfliktthemen (nach Luborsky) bei Patienten mit generalisierter Angststörung." Doctoral thesis, 2013. http://hdl.handle.net/11858/00-1735-0000-0019-859F-4.

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Beltrán, Varas Víctor Javier. "Bewertung endoskopischer Verfahren in der Oralchirurgie nach 15 Jahren Anwendung." Doctoral thesis, 2016. http://hdl.handle.net/11858/00-1735-0000-0028-86FD-6.

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Ziel der vorliegenden Arbeit war eine Analyse der Entwicklung der Endoskopie im Bereich der dentoalveolären Chirurgie am Zentrum ZMK-Heilkunde der Universitätsmedizin Göttingen. Zu diesem Zwecke wurden die im OP - Register verzeichneten endoskopischen Eingriffe der Jahre 1997-2012 ausgewählt. In dieser Gesamtgruppe (Kohorte) wurden demografische Parameter und die anatomische Lokalisation der Eingriffe ermittelt. Aus dem Archiv wurden videoendoskopische Aufzeichnungen für weitergehende Auswertungen ausgewählt und ausgewertet: Klinisch diagnostische Maßnahmen (Subgruppe A, Stützendoskopie, n

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Nowak, Kathrin Annelore. "Korrektur der Fallotschen Tetralogie nach vorhergehender Palliativoperation- Langzeitergebnisse aus einem historischen Patientenkollektiv." Doctoral thesis, 2016. http://hdl.handle.net/11858/00-1735-0000-0028-874D-A.

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Korrektur der Fallotschen Tetralogie nach vorhergehender Palliativoperation - Langzeitergebnisse aus einem historischen Patientenkollektiv Hintergrund: Die Fallotschen Tetralogie ist ein komplexer zyanotischer Herzfehler, der erst mit dem Einsatz der Herz-Lungen-Maschine korrigiert werden kann. Zuvor erfolgte eine palliativ Operation. Seit 1960 werden Patienten mit Fallotscher Tetralogie in der Klinik für Thorax, -Herz- und Gefäßchirurgie der Universität Göttingen operiert. Ziel der Arbeit ist es, die Langzeitergebnisse eines historischen Patientenkollektivs, die zwischen 1960 und 1984 zuerst

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Peitsch, Werner Karl Josef. "Komplikationen nach endoskopisch-laparoskopischer Hernioplastik (TAPP) als Regeloperation zur Versorgung von Leistenhernien." Doctoral thesis, 2013. http://hdl.handle.net/11858/00-1735-0000-001D-BF71-8.

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