Metallpniktide und -chalkogenide erfahren zunehmend mehr Aufmerksamkeit in Chemie und Festkörperphysik. Dieses Interesse liegt unter anderem in der ungewöhnlichen Strukturchemie der Verbindungen begründet. In den Pniktogen(Pn)- bzw. Chalkogen(Q)-reichen Verbindungen dieser Systeme ist besonders häufig die Bildung der jeweiligen Oligo- oder Polyanionen bzw. Moleküle zu beobachten. Einerseits können die homoatomaren Pn–Pn- bzw. Q–Q-Bindungen zur Ausbildung niederdimensionaler Strukturmotive mit anisotropen Eigenschaften, wie bspw. Supraleitung und Metall-Halbleiter-Übergänge, führen; andererseits ergeben sich aus dem sterischen Raumanspruch der Struktureinheiten in Kombination mit den hohen Koordinationszahlen schwerer Übergangs- oder Actinoidmetalle komplexe Strukturen. Die Pn- bzw. Q-Atome treten häufig gemischtvalent auf, was zusammen mit den beschriebenen Strukturmerkmalen die enorme Variabilität und Anpassungsfähigkeit dieser Stoffsysteme widerspiegelt. Im Rahmen des ersten Teils der vorliegenden Dissertation wurde die potentielle Oligoanionenbildung in den bisher als quadratisch-planar beschriebenen Phosphidschichten von Actinoidphosphidtelluriden diskutiert. Über eine chemische Transportreaktion mit Iod ist es gelungen Kristalle des Uranphosphidtellurids UPTe und des verwandten, bisher unbekannten Diuranphosphidditelluridoxids U2PTe2O zu züchten und die Kristallstrukturen durch Einkristallröntgendiffraktometrie aufzuklären. Die Strukturen beider Verbindungen können durch eine Abfolge von [U2P2]- und [Te2]-Schichten, bzw. [U2P2]-, [U2O2]- und [Te2]-Schichten entlang [001] beschrieben werden. Die Phosphoratome in den [U2P2]-Abschnitten bilden eine Schicht parallel ausgerichteter P2-Anionen. Die Zusammenlagerung der Phosphoratome sowie die geordnete Ausrichtung der Hanteln bedingt eine Symmetriereduktion der ursprünglich tetragonal angenommenen Struktur mit fehlgeordneten Phosphoratomen hin zu einem Strukturmodell in der monoklinen Raumgruppe I11m. Bindungsanalysen im Realraum mit Hilfe des Elektronen-Lokalisierbarkeits-Indikator (ELI D) ergaben für UPTe in der monoklin verzerrten Struktur ein zusätzliches Doppelmaximum auf der gedachten Linie zwischen den Phosphoratomen P1 und P2, welches als homoatomare P–P-Bindungen interpretiert werden kann. Zudem konnte über eine Festkörpersynthese die ternäre Verbindung Thoriumphosphidtellurid ThPTe erhalten werden, deren Pulverröntgendaten ein zu UPTe analoges Strukturbild zeigt. Wenngleich die Fehlordnung in der Phosphorschicht von ThPTe experimentell nicht aufgelöst werden konnte, war es durch Raman-Spektroskopie möglich, die Existenz der P2 Hanteln sowohl in ThPTe als auch in UPTe zu belegen. Beide isotype Verbindungen können in ionischer Grenzschreibweise als A4+ + ½ P24– + Te2– (A = Th, U) formuliert werden. Im zweiten Teil der vorliegenden Dissertation wurde die vielfältige Strukturchemie neuer Selen-Halogenid-Komplexe des Iridiums insbesondere hinsichtlich ihrer Oligoselenidliganden sowie koordinativ gebundener Selenmoleküle dargelegt. Durch die Aktivierung von elementarem Iridium in Selentetrahalogenid-Schmelzen konnten erstmalig Verbindungen im System Ir–Se–Br dargestellt und die Strukturvielfalt im System Ir–Se–Cl signifikant erweitert werden. Die synthetisierten ein- bis achtkernigen Iridium(III)-Komplexe zeichnen sich durch eine bemerkenswerte Diversität ihrer Liganden aus, die von Halogenidionen, Selenmono- und Selendihalogenid-Einheiten über zyklische Selenmoleküle bis zu Oligoselenidketten reicht. Die variablen Verknüpfungsmoden dieser Liganden erweitern zusätzlich das Spektrum möglicher Komplexformen und -größen. Die kleinsten, dargestellten ternären Iridiumkomplexe a-fac-[IrBr3(SeBr2)3], m-fac-[IrBr3(SeBr2)3] und mer-[IrBr3(SeBr2)3] besitzen ausschließlich endständige Selendibromid- und Bromidliganden, die sich in ihrer Konfiguration unterscheiden. In den isotypen, zweikernigen Iridiumkomplexen [Se9(IrX3)2] (X = Cl, Br, Cl/Br) wird ein ungeladener, unter den Allotropen des Selens unbekannter Se9-Ring in Kronen-Konformation durch zwei IrX3-Moleküle stabilisiert. Der cyclo-Nonaselenligand ist der erste seiner Art, der mittels Röntgenbeugung am Einkristall charakterisiert werden konnte. Se9(IrCl1.66(1)Br1.34(1))2 repräsentiert zudem die erste quaternäre Verbindung in den Systemen M–Se–Cl–Br (M = Platinmetalle). Die ringförmigen, vier- und sechskernigen Komplexe [Ir4Se10Br16] sowie [Ir6Se8Cl30] und [Ir6Se6Cl30] zählen zu den größten Ringstrukturen unter den Chalkogen-Halogeniden der Platinmetalle. Ihre intramolekulare Verknüpfung wird unter anderem durch µ-verbrückende X–-Anionen und sehr seltene (SeX)–-Einheiten realisiert. Die verwandten [Ir6Se8Cl30]- und [Ir6Se6Cl30]-Ringe können als molekularer Ausschnitt der aus [IrCl6/2]-Oktaedern bestehenden Honigwabenstruktur von alpha-IrCl3 beschrieben werden. Die achtkernigen Iridiumkomplexe [Ir8Se28Br14] und [Ir8Se40Br10] bilden über die sechsfach-verbrückenden Se22–-Hanteln und die vierfach-verbrückenden Se42–-Ketten sehr große, ellipsoide Moleküle aus, die stark einem Ausschnitt aus der Netzwerkstruktur von Ir3Se8 ähneln. Beide Komplexe unterscheiden sich lediglich in ihren apikal koordinierenden Liganden: SeBr2-Einheiten im Fall von [Ir8Se28Br14] und ungeladene Heptaselenringe im Fall von [Ir8Se40Br10]. Die Se7-Moleküle repräsentieren ihrerseits die ersten cyclo-Heptaseleneinheiten in Boot-Konformation. An den [Ir8Se28Br14] Komplex koordinieren über Wasserstoffbrückenbindungen zusätzlich zwei Wassermoleküle. Die räumliche Anordnung der Moleküle im Festkörper von Ir8Se28Br14·2H2O stellt eine hervorragende Näherung der dichtesten Ellipsoidpackung dar.

Dans cette thèse, on vise deux types d'applications de l’antenne à résonateur diélectrique (DRA): 1) La réalisation d’un élément rayonnant pour un réseau phasé embarqué sur un véhicule terrestre ou un avion. Cet élément de base requiert une couverture en élévation supérieure à celle des éléments imprimés pour permettre une poursuite typique comprise entre ±70°. La couverture dans un cône large est assurée avec une bonne pureté de polarisation circulaire en alimentant l’antenne à travers deux ouvertures à fente en H orthogonales parfaitement découplées en bande X. 2) La deuxième structure est destinée à la diversité d’antennes dans le contexte des réseaux corporels embarqués ou Body Area Network (BAN). L’antenne à diversité combine une antenne fente en boucle avec un DRA ce qui permet dans un espace compact de réaliser des diagrammes de type “broadside” et “endfire” respectivement. Les alimentations considérées sont de 2 types; Soit purement planaire (microruban et coplanaire) soit mixte en combinant une alimentation coaxiale et une alimentation coplanaire. Caractéristiques principales des antennes à résonateur diélectrique (DRA): Pour répondre aux attentes des utilisateurs en termes de débit, les systèmes de communication sans fils se tournent vers des fréquences de plus en plus élevées. La conséquence de cette montée en fréquence est notamment l’augmentation des pertes au niveau des éléments conducteurs et donc une diminution de l’efficacité globale des systèmes de communication. Dans ces circonstances, les DRA offre de meilleurs résultats par rapport à d'autres familles d'antennes à base d’éléments métalliques. De plus, les DRA offrent des pertes diélectriques négligeables, elles sont peu sensibles aux variations de température et s’intègrent facilement sur des technologies de fabrication planaires / Technologies such as direct broad cast satellite system (DBSS), Geosynchronous Earth Orbit (GEO) and Low Earth Orbit (LEO) satellite communications , global positioning system (GPS), high accuracy airborne navigation system and a large variety of radar systems demand for high level of antenna performance. Similar is the requirement for upcoming land based wireless systems such as cellular and indoor communication systems that is needed some more specific and additional features added to the antenna to compensate for the deficiencies encountered in system's performance. Though metallic antennas are capable enough to fulfil all the operational requirements, however at very high frequencies and under hostile temperature conditions they are constrained to face certain limitations. To avoid these constraints the performance of Dielectric Resonator Antennas (DRAs) is evaluated and their new applications are proposed. In the thesis, two types of antenna applications are sought :-First is for tracking and satellite applications that needs a larger aperture coverage in elevation plane. This coverage is realized with a good CP purity by proposing two ports dual linearly polarized DRA working at X-band. The DRA is excited by two orthogonal H-shaped aperture slots yielding two orthogonal polarizations in the broadside direction. A common impedance bandwidth of 5.9% and input port isolation of -35 dB are obtained. The broadside radiation patterns are found to be highly symmetric and stable with cross polarization levels -15dB or better over the entire matching frequency band. The maximum measured gain is found to be 2.5dBi at 8.4 GHz.- The 2nd type of antenna is a dual pattern diversity antenna to be used in the Body Area Network (BAN) context. This antenna combines a slot loop and DRA yielding broadside and end-fire radiation patterns respectively. Based upon the feeding techniques, the DG antenna is further divided into two categories one with planar feeds and the other with non-planar feeds (slot loop excited by planar CPW but DRA excited by vertical monopole) .Both types are successfully designed and measured upon body when configured into different propagation scenarios. The non-planar feeds antenna allows wider common impedance bandwidths than the planar feeds (4.95% vs 1.5%).In both cases, a maximum value of DG=9.5dB was achieved when diversity performance tests were carried out in rich fading environments. This value is close to the one (10 dB) theoretically reached in a pure Rayleigh environment and was obtained with efficiencies of 70% and 85% for the slot loop and the DRA respectively. Therefore, we conclude that these antennas could be used on the shoulders or the chest of professional clothes (firemen, policemen, soldier) where full planar integration is not a key issue but where the communication must be efficient in harsh environments and for various gestures, positions and scenarios

The effects of metastable tetragonal zirconia on the properties of Ordinary Portland Cement were observed during which the effect of crystallite size pH on the preparation solution, precursor salt, and the presence of co-precipitates, Fe(OH)3, SnO2 and SiO2 on the crystallization temperature, enthalpy and crystal structure, immediately following the crystallization exothermic burst phenomenon in ZrO2 were measured. Thermal analysis and x-ray methods were used to determine crystallite sizes and structures immediately following the exothermic burst. Comparisons were made for zirconias prepared from oxychloride, chloride and nitrate solutions. The existence of tetrameric hydroxidecontaining ions in oxychloride precursor is used to rationalise low values of crystallization enthalpy. The position of the crystallization temperature, Tmax was not dependent on crystallite size alone but also on the pH at which the gel was made, the surface pH after washing, and the presence of diluent oxides. Enthalpy v r1/2 and Tmax v (diluent vol)1/3 relationships indicate that surface coverage effects dominate a surface nucleated phenomenon. The data established for ZrO2 systems was used to develop tetragonal-ZrO2-SnO2 powders capable of improving the mechanical properties of Ordinary Portland Cement discs. The ZrO2-OPC discs were prepared by powder mixing, water hydration and uniaxial pressing. Vicat needle tests showed that tetragonal-ZrO2 increases the initial setting rate. Microscopy indicated that porosity distribution changes near to ZrO2 particles. Zirconia has also been introduced into OPC discs by vacuum infiltration methods developed for solutions and colloidal suspensions. Comparisons between OPC discs and the OPCtetragonal ZrO2 composites have been made on the basis of diametral compression strength, Young’s modulus, hardness and toughness (K1c), as estimated by the cracked indentation method. Bell-shaped curves are found for the way the mechanical properties are changed as a function of Zirconia content.

Neste trabalho consideramos três tópicos principais. Nos dois primeiros generalizamos alguns dos resultados clássicos da Teoria da Confiabilidade na otimização dos procedimentos de burn-in e de políticas de garantia, respectivamente, sob o modelo de tempo de vida geral, quando um sistema coerente é observado ao nível de seus componentes, e estendemos os conceitos de intensidade de falha na forma de banheira e do modelo de falha geral através da definiçâo de processos progressivamente mensuráveis sob a pré-t-história completa dos componentes do sistema. Uma regra de parada monótona é usada na metodologia de otimizaçâo proposta. No terceiro tópico modelamos os custos de garantia descontados por reparo mínimo de um sistema coerente ao nível de seus componentes, propomos o estimador martingal do custo esperado para um período de garantia fixado e provamos as suas propriedades assintóticas mediante o Teorema do Limite Central para Martingais. / In this work we consider three main topics. In the first two, we generalize some classical results on Reliability Theory related to the optimization in burn-in procedures and warranty policies, using the general lifetime model of a coherent system observed on the component level and extending the definitions of bathtub shaped failure rate and general failure model to progressively measurable processes under the complete pre-t-history. A monotone stopping rule is applied within the proposed methodology. In the third topic, we define the discounted warranty cost process for a coherent system minimally repaired on the component level and we propose a martingale estimator to the expected warranty cost for a fixed period and setting its asymptotic properties by means of Martingale Central Limit Theorem.

Neste trabalho consideramos três tópicos principais. Nos dois primeiros generalizamos alguns dos resultados clássicos da Teoria da Confiabilidade na otimização dos procedimentos de burn-in e de políticas de garantia, respectivamente, sob o modelo de tempo de vida geral, quando um sistema coerente é observado ao nível de seus componentes, e estendemos os conceitos de intensidade de falha na forma de banheira e do modelo de falha geral através da definiçâo de processos progressivamente mensuráveis sob a pré-t-história completa dos componentes do sistema. Uma regra de parada monótona é usada na metodologia de otimizaçâo proposta. No terceiro tópico modelamos os custos de garantia descontados por reparo mínimo de um sistema coerente ao nível de seus componentes, propomos o estimador martingal do custo esperado para um período de garantia fixado e provamos as suas propriedades assintóticas mediante o Teorema do Limite Central para Martingais. / In this work we consider three main topics. In the first two, we generalize some classical results on Reliability Theory related to the optimization in burn-in procedures and warranty policies, using the general lifetime model of a coherent system observed on the component level and extending the definitions of bathtub shaped failure rate and general failure model to progressively measurable processes under the complete pre-t-history. A monotone stopping rule is applied within the proposed methodology. In the third topic, we define the discounted warranty cost process for a coherent system minimally repaired on the component level and we propose a martingale estimator to the expected warranty cost for a fixed period and setting its asymptotic properties by means of Martingale Central Limit Theorem.

L'hématopoïèse regroupe les phénomènes menant à la formation des composantes<br />cellulaires du sang. Au cours de ce processus, des cellules précurseurs vont proliférer et se<br />différencier dans les multiples types cellulaires spécialisés. Le développement du système<br />hématopoïétique de la Drosophile et des vertébrés présente de nombreuses similitudes aussi bien<br />au niveau fonctionnel et ontogénique qu'au niveau des gènes qui régulent la formation des<br />cellules sanguines. Chez la Drosophile, au stade embryonnaire, les précurseurs<br />hématopoïétiques, les prohémocytes, vont générer deux types de cellules sanguines, les<br />plasmatocytes et les cellules à cristaux. Nous avons entrepris de caractériser les mécanismes de<br />régulation de l'hématopoïèse embryonnaire chez la Drosophile.<br />Dans un premier temps, nous avons analysé la fonction et le mode d'action du facteur de<br />transcriptions de type GATA Serpent (Srp) au cours de ce processus. Nous avons mis en<br />évidence que le gène serpent code pour deux isoformes qui ont des activités différentielles au<br />cours de ce processus. D'autre part, nous avons montré que l'activité de Srp au cours de<br />l'hématopoïèse est modulée par recrutement de cofacteurs. Ainsi, nous avons montré que Srp est<br />capable de recruter U-Shaped, un cofacteur de type FOG (Friend Of GATA), mais aussi, de<br />former un complexe fonctionnel avec le facteur de transcription de type RUNX, Lozenge. La<br />caractérisation des isoformes de Srp et la mise en évidence de l'interaction de ce facteur GATA<br />avec différents partenaires a permis de mettre en évidence la versatilité des fonctions de srp au<br />cours de l'hématopoïèse.<br />Dans un second temps, nous avons entrepris de caractériser in vivo l'étape de ségrégation<br />des deux populations, plasmatocytes et cellules à cristaux. Nous avons mis en évidence que la<br />ségrégation de ces deux lignages à partir d'une population de prohémocytes bipotents est un<br />processus très dynamique, contrôlé par un mécanisme original en deux étapes. Cette régulation<br />qui fait intervenir les facteurs de transcription lignage-spécifiques Lozenge et Glial-Cell-<br />Missing (Gcm) et Gcm2, contrôle précocement la détermination des précurseurs et tardivement<br />le maintient de l'identité de ces cellules dans les phases de différenciation en cellules à cristaux<br />versus plasmatocytes. De manière intéressante, nous avons montré que la régulation de la<br />ségrégation, ne repose pas sur un antagonisme réciproque entre les facteurs de transcription<br />lignage-spécifiques. Ce mécanisme qui contrôle l'acquisition d'un destin cellulaire diffère donc<br />des processus de régulation de l'hématopoïèse mis en évidence chez les mammifères.

Synthetic and degradable polymers are an attractive choicein many areas, since it is possible to control the way in whichthey are manufactured; more specifically, pathways tomanipulate the architecture, the mechanical properties and thedegradation times have been identified. In this work,L-lactide, 1,5-dioxepan-2-one and ε-caprolactone were usedas monomers to synthesize polymers with different architecturesby ring-opening polymerization. By using novel initiators,triblock copolymers, functionalized linear macromonomers andstar-shaped aliphatic polyesters with well-defined structureshave been synthesized. To synthesize triblock copolymers,cyclic germanium initiators were studied. The polymerizationproceeded in a controlled manner although the reaction rateswere low. To introduce functionality into the polymer backbone,functionalized cyclic tin alkoxides were prepared and used asinitiators. During the insertion-coordination polymerization,the initiator fragment consisting mainly of a double bond wasincorporated into the polymer backbone. The double bond wasalso successfully epoxidized and this gave unique possibilitiesof synthesizing graft polymers with precise spacing. Themacromonomer technique is a very effective method for producingwell-defined graft polymers. Spirocyclic tin initiators weresynthesized and used to construct star-shaped polymers. Thestar-shaped polymers were subsequently crosslinked in apolycondensation reaction. These crosslinked structures swelledin water, and swelling tests showed that by changing thestructure of the hydrogel network, the degree of swelling canbe altered. A first evaluation of the surface characteristicsof the linear triblock copolymers was also performed. AFManalysis of the heat-treated surfaces revealed nanometer-scalefibers and tests showed that keratinocytes were able to growand proliferate on these surfaces. / QC 20100602

Grave X was found in 1952 during construction work in Tuna in Badelunda parish, in the province of Västmanland. Objects from this 3rd Century grave were dispersed and the stone grave covering and cist-like wooden burial chamber were cut almost in half as a result of the construction work that unearthed it. The purpose of this dissertation is to create a better understanding of Tuna in Badelunda and to place Grave X and the person buried there in context. Due to my interest in Grave X and the person in this grave, the scope of the study is limited to Tuna during the Late Roman Iron Age. What kind of place may Tuna in Badelunda have been during that time? Which kinds of knowledge may the person in Grave X have possessed and what roles may this person have had in local society? How may this person have acted in Tuna in Badelunda in particular? Why was this person buried in the specific type of structure that was Grave X? To answer these questions, ancient monuments and phenomena in the Tuna area, objects from the grave and construction details of the grave are discussed. Specifically, I examine the name Tuna, stone enclosures, hillforts of Bejby borg-character and travel routes, beads, golden rings in the shape of snakes, vessels and serving utensils, and the stone grave covering and cist-like chamber. Since Grave X was partly ruined when discovered, comparisons are made to about 20 similar graves from other parts of Scandinavia in order to get an idea of what may have been lost from Grave X. A performative-constructive gender perspective is of importance in this dissertation, as well as the concept of creolization. The kinds of knowledge and the societal roles the person in Grave X may have had can be summarized in five categories or contexts of action: production within the (social-political) economy of the farm, ritual performances, physical communication, textile production, and oral performances with the telling of stories and relating of memories. Possible personal strategies in relation to the activities the person in question was involved in are seen as important. One way this dissertation takes up this subject is through the discussion of the role the person may have had in greetings and farewells in the yard of the farm (Sw. tun, gårdsplan). Greetings and farewells were probably of importance, and Tuna is discussed as a crossroads. This means that although a local perspective is advocated in this dissertation, Tuna may not be seen as an isolated community, but rather as a small place that to a great extent partook in the larger world. This can also be seen in Grave X; when the person in this grave was buried, the living made choices that both expressed local traditions and made reference to far-away places. In contrast to the surrounding graves, the person in Grave X was not cremated. One of many possible reasons may have been a desire to emphasize the person’s personality and gender as well as roles in society. / <p>Auktoriserad namnform i LIBRIS: Fernstål, Charlotte, 1974-</p>

The pseudospin symmetry concept is investigated by solving the Dirac equation for the exactly solvable potentials such as pseudoharmonic potential, Mie-type potential, Woods-Saxon potential and Hulth&eacute / n plus ring-shaped potential with any spin-orbit coupling term $kappa$. Nikiforov-Uvarov Method, Asymptotic Iteration Method and functional analysis method are used in the calculations. The energy eigenvalue equations of the Dirac particles are found and the corresponding radial wave functions are presented in terms of special functions. We look for the contribution of the ring-shaped potential to the energy spectra of the Dirac particles. Particular cases of the potentials are also discussed. By considering some particular cases, our results are reduced to the well-known ones presented in the literature. In addition, by taking equal mixture of scalar and vector potentials together with tensor potential, solutions of the Dirac equation are found and then the energy splitting between the two states in the pseudospin doublets is investigated. We indicate that degeneracy between members of pseudospin doublet is removed by tensor interactions. Effects of the potential parameters on the pseudospin doublet splitting are also studied. Radial nodes structure of the Dirac spinor are presented.

Hypersonic vehicles are exposed to severe heating loads during their flight in the atmosphere. In order to minimize the heating problem, a variety of cooling techniques are presently available for hypersonic blunt bodies. Introduction of a forward-facing cavity in the nose tip of a blunt body configuration of hypersonic vehicle is one of the most simple and attractive methods of reducing the convective heating rates on such a vehicle. In addition to aerodynamic heating, the overall drag force experienced by vehicles flying at hypersonic speeds is predominate due to formation of strong shock waves in the flow. Hence, the effective management of heat transfer rate and aerodynamic drag is a primary element to the success of any hypersonic vehicle design. So, precise information on both aerodynamic forces and heat transfer rates are essential in deciding the performance of the vehicle. In order to address the issue of both forces and heat transfer rates, right kind of measurement techniques must be incorporated in the ground-based testing facilities for such type of body configurations. Impulse facilities are the only devices that can simulate high altitude flight conditions. Uncertainties in test flow conditions of impulse facilities are some of the critical issues that essentially affect the final experimental results. Hence, more reliable and carefully designed experimental techniques/methodologies are needed in impulse facilities for generating experimental data, especially at hypersonic Mach numbers. In view of the above, an experimental program has been initiated to develop novel techniques of measuring both the aerodynamic forces and surface heat transfer rates. In the present investigation, both aerodynamic forces and surface heat transfer rates are measured over the test models at hypersonic Mach numbers in IISc hypersonic shock tunnel HST-2, having an effective test time of 800 s. The aerodynamic coefficients are measured with a miniature type accelerometer based balance system where as platinum thin film sensors are used to measure the convective heat transfer rates over the surface of the test model. An internally mountable accelerometer based balance system (three and six-component) is used for the measurement of aerodynamic forces and moment coefficients acting on the different test models (i.e., blunt cone with after body, blunt cone with after body and frustum, blunt cone with after body-frustum-triangular fins and sharp cone with after body-frustum-triangular fins), flying at free stream Mach numbers of 5.75 and 8 in hypersonic shock tunnel. The main principle of this design is that the model along with the internally mounted accelerometer balance system are supported by rubber bushes and there-by ensuring unrestrained free floating conditions of the model in the test section during the flow duration. In order to get a better performance from the accelerometer balance system, the location of accelerometers plays a vital role during the initial design of the balance. Hence, axi-symmetric finite element modeling (FEM) of the integrated model-balance system for the missile shaped model has been carried out at 0° angle of attack in a flow Mach number of 8. The drag force of a model was determined using commercial package of MSC/NASTRAN and MSC/PATRAN. For test flow duration of 800 s, the neoprene type rubber with Young’s modulus of 3 MPa and material combinations (aluminum and stainless steel material used as the model and balance) were chosen. The simulated drag acceleration (finite element) from the drag accelerometer is compared with recorded acceleration-time history from the accelerometer during the shock tunnel testing. The agreement between the acceleration-time history from finite-element simulation and measured response from the accelerometer is very good within the test flow domain. In order to verify the performance of the balance, tests were carried out on similar standard AGARD model configurations (blunt cone with cylinder and blunt cone with cylinder-frustum) and the results indicated that the measured values match very well with the AGARD model data and theoretically estimated values. Modified Newtonian theory is used to calculate the aerodynamic force coefficient analytically for various angles of attack. Convective surface heat transfer rate measurements are carried out by using vacuum sputtered platinum thin film sensors deposited on ceramic substrate (Macor) inserts which in turn are embedded on the metallic missile shaped body. Investigations are carried out on a model with and without fin configurations in HST-2 at flow Mach number of 5.75 and 8 with a stagnation enthalpy of 2 MJ/kg for zero degree angle of attack. The measured heating rates for the missile shaped body (i.e., with fin configuration) are lower than the predicted stagnation heating rates (Fay-Riddell expression) and the maximum difference is about 8%. These differences may be due to the theoretical values of velocity gradient used in the empirical relation. The experimentally measured values are expressed in terms of normalized heat transfer rates, Stanton numbers and correlated Stanton numbers, compared with the numerically estimated results. From the results, it is inferred that the location of maximum heating occurs at stagnation point which corresponds to zero velocity gradient. The heat-transfer ratio (q1/Qo)remains same in the stagnation zone of the model when the Mach number is increased from 5.75 to 8. At the corners of the blunt cone, the heat transfer rate doesn’t increase (or) fluctuate and the effects are negligible at two different Mach numbers (5.75 and 8). On the basis of equivalent total enthalpy, the heat-transfer rate with fin configuration (i.e., at junction of cylinder and fins) is slightly higher than that of the missile model without fin. Attempts have also been made to evaluate the feasibility of using forward facing cavity as probable technique to reduce the heat transfer rate and to study its effect on aerodynamic coefficients on a 41° apex angle missile shaped body, in hypersonic shock tunnel at a free stream Mach number of 8. The forward-facing circular cavities with two different diameters of 6 and 12 mm are chosen for the present investigations. Experiments are carried out at zero degree angle of attack for heat transfer measurements. About 10-25 % reduction in heat transfer rates is observed with cavity at gauge locations close to stagnation region, whereas the reduction in surface heat transfer rate is between 10-15 % for all other gauge locations (which is slightly downstream of the cavity) compared with the model without cavity. In order to understand the influence of forward facing cavities on force coefficients, measurement of aerodynamic forces and moment coefficients are also carried out on a missile shaped body at angles of attack. The same six component balance is also being used for subsequent investigation of force measurement on a missile shaped body with forward facing cavity. Overall drag reductions of up to 5 % is obtained for a cavity of 6 mm diameter, where as, for the 12 mm cavity an increase in aerodynamic drag is observed (up to about 10%). The addition of cavity resulted in a slight increase in the missile L/D ratio and did not significantly affect the missile lateral components. In summary, the designed balances are found to be suitable for force measurements on different test models in flows of duration less than a millisecond. In order to compliment the experimental results, axi-symmetric, Navier-Stokes CFD computations for the above-defined models are carried out for various angles of attack using a commercial package CFX-Ansys 5.7. The experimental free stream conditions obtained from the shock tunnel are used for the boundary conditions in the CFD simulation. The fundamental aerodynamic coefficients and heat transfer rates of experimental results are shown to be in good agreement with the predicted CFD. In order to have a feeling of the shock structure over test models, flow visualization experiments have been carried out by using the Schlieren technique at flow Mach numbers of 5.75 and 8. The visualized shock wave pattern around the test model consists of a strong bow shock which is spherical in shape and symmetrical over the forebody of the cone. Experimentally measured shock stand-off distance compare well with the computed value as well as the theoretically estimated value using Van Dyke’s theory. These flow visualization experiments have given a factual proof to the quality of flow in the tunnel test section.