In order to ensure safe travel, railway vehicles must be stable under every condition along the track. Thus, a vehicle can be certified for operation only when it can fulfil certain criteria related to the ride stability. The stability of the vehicle is highly dependent on the wheel-rail friction coefficient: higher friction results in worse ride. So, to ensure a good evaluation of the stability, the friction should be high enough during tests. The same applies to the risk of wheel flange climbing. At the present time, the wheel-rail friction can not be measured directly but there are different procedures utilized to ensure that the conditions are suitable for testing the stability of the vehicle. In this study an algorithm is proposed to estimate the wheel-rail friction coefficient by using quantities which can be measured in reality. The algorithm is tried out in computer simulations. The algorithm has two parts: in Part 1 the friction coefficient is proposed to be equal to the ratio of the total creep force divided by the normal force; in Part 2 the total creep and spin creep are estimated to observe their correlation to the estimated friction. The contact angle in Part 1 is estimated by a contact point function. In the simulations, different conditions are tried. There are four horizontal radii: tangent track, R1300m, R1000m, and R400m. Three friction coefficients are used: 0.5, 0.4 and 0.3. In addition to this, track irregularities are included. A single vehicle is simulated in two modes: capable and incapable of passive radial steering. The track irregularities caused high values of the proposed estimated friction coefficient. The values in some instances were close or equal to the input friction coefficient of the simulation. Thus, if the highest values of the estimated friction were taken over a certain distance or time, the friction of the simulation could be approximated. In most cases, the total creep was following the trend of the estimated friction. The total creep and spin creep were used as a quality factor to determine how close the estimated friction was to the simulation’s friction. In this study when the total creep was greater than 0.006 and the spin creep was less than 1.0 m-1, the estimated friction was close to the input friction. The closeness was dependent on the simulation’s friction. Higher input friction resulted in larger deviation compared to lower friction. A sensitivity analysis has been performed by deliberately introducing errors in the position of the contact point and the angle of attack. The analysis shows that the errors are not critical when the contact point is close to the tread circle. When the contact point is close to the flange, a good measurement of the wheel profile and the contact point position required to obtain accurate results. On the other hand, the errors affect the friction estimate for high spin and low total creepage. These results are discarded by the algorithm, the influence of the errors is minimized.

A swirl injector for a rocket engine being developed by \emph{AESIR} (Association of EngineeringStudents in Rocketry) was simulated with different geometric parameters. The swirl injector is usedto atomize the ethanol used as fuel and to create a spray that mixes well with the oxidizer withinthe combustion chamber. Inlet slot angle (90, 75, 60 and 45 degrees), swirl chamber length (15, 20and 25 mm) and outlet orifice diameter (3, 6 and 9 mm) were examined.Previous studies in swirl injectors show that CFD can be used to analyze the flow in such aninjector, furthermore theoretical models exist that can predict some of the general characteristicsof the flow. Previous studies have also simulated transient behavior and flow features effectingbreakup of fuel flowing through a swirl injector.A steady state simulation using Volume of Fluid (VOF) multiphase modeling and $k$-$\omega$ \emph{SST}turbulence modeling was used to simulate the swirl injector intended for the rocket engine. It wasfound that a wider outlet orifice would give a wider cone angle of spray. This is desirable in thecurrent rocket engine design as it will promote greater mixing of fuel and oxidizer higher up in thecombustion chamber. No large variances was observed when different inlet slot angles was simulated. Ashorter swirl chamber length reduced the amount of losses in energy due to viscous forces. The flowafter the outlet orifice was not simulated so the effect of turbulence kinetic energy and energylosses outside of the swirl injector have not been analyzed, previous studies have indicated thatturbulent kinetic energy does have an effect on the breakup and atomization of the fuel.It was concluded that using a wider outlet orifice of 9 mm gave the best results out of the differentgeometric parameters analyzed and the swirl chamber length should be a short as possible.

One idea to stop the increasing threat of global warming is to build a space sunshade, made up of a constellation of satellites to reflect a portion of the sunlight. These satellites need to reach an equilibrium point where they can stay in orbit with minimal adjustments. A few feasibility studies have been made in this area and the location of the equilibrium point, L1' has been found. An area that is still unclear is the best way of getting the satellites to L1'. One idea is to use electric propulsion engines , and utilizing a gravity assist around the Moon on the way to L1'. Gravity assists have mostly been performed with chemical rocket engines, so doing it with electric propulsion causes some unique issues. The goal was to find a trajectory including the gravity assist showing that this could be an effective way of transporting the satellites. To measure how effective this would be, a trajectory without a gravity assist was also created as a means of comparison. The trajectory and orbit simulations were done in the program General Missions Analysis Tool (GMAT), and the resulting trajectory took 51 days and used 83.4kg of fuel for a fuel-to-mass-ratio of 21.5%. This was a worse result compared to the trajectory without a gravity assist, which only used 80.4kg of fuel. Finally a discussion around a potential trajectory which was shown to have a much greater velocity increase was had, which would indicate that a gravity assist maneuver could provide a trajectory that does save on fuel compared to using no gravity assist.

The evolution of electronics in the vehicle industry has introduced the possibility for more X-by-wire systems in future vehicles. However, the use of steer-by-wire systems has not yet been widelyimplemented. This opens up an opportunity to explore strategies around the potential use of such asystem.The purpose of the project was to evaluate how to design a variable steering ratio which would give asuitable ratio in all speeds. This would, in turn, make it possible to reduce the need for large steeringwheel angles. Additionally, steering wheel designs which can be implemented with a steer-by-wiresystems are discussed and what possibilities there are to move certain interfaces to the steering wheel.The evaluation process consisted of driving a real car with a constant steering ratio in normal trafficand later modelling a variable steering ratio and testing it in a simulator. This was to get data on howlarge steering wheel angles that are needed in different driving scenarios to then be able to design asuitable variable steering ratio. The tests conducted on normal roads in a real car has shown that thedriver utilises the whole steering range (full lock-lock distance) at speeds below 30 km/h and about±10° on the steering wheel at high speeds. The tests conducted in the simulator show that the variablesteering ratio presented in this report decreases the workload on the driver most of all at speeds below30 km/h.The variable steering ratio presented has been compared with a fixed steering ratio in the simulatorand the tests show that the variable steering ratio works similar to the fixed steering ratio in the samescenarios. The variable steering ratio also decreases the need for a steering wheel angle greater than±180°.

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This volume covers the phases from design to manufacturing of a wind tunnel testsupport structure for a conceptual blended wingbodyUAV designed by KTH GreenRaven Project students. The innovative aircraft design demonstrates sustainabilitywithin aviation by utilizing a hybrid electricfuelcell propulsion system. The windtunnel test to be conducted at Bristol University will produce data to evaluate theaerodynamic properties of the model for design verification. The wind tunnel modelis a smallscaled1.5mspanmodel supported by struts that change the pitch andyaw angles during testing. An external force balance provided by Bristol Universitymeasures the loads and moments experienced by the model. The main requirementsfor the structure are to withstand the aerodynamic loads imposed by the model andto change the model’s orientation while maintaining wind speed during the test. Themaximum aerodynamic loads were provided in a matrix, the largest of which was usedas the load condition for the support equating to a 512N lift at 14◦ AOA. Trade studieswere conducted to determine the mechanisms to satisfy the requirements while stayingwithin budget. The chosen design for the support structure includes a circular baseplate constrained by a locking ring with positioning pins to change the yaw angle. Themain strut is mounted at the the center of the circular base plate. A hinge bracketat the top of the strut interfaces with another hinge bracket within the model viaa clevis pin. An electric linear actuator mounted downstream of the main strut isused to vary the pitch angle, with the center of rotation at the clevis pin. Once thedesign was finalized, finite element analysis was done to verify the structural stabilityof the design. The FEA results were compared to EulerBernoulliapproximations fordeflection. Manufacturing of the components was outsourcedwhile assembly andprogramming of the actuator was done inhouse. / Det här examensarbetet är en del av ett projekt som omfattar processen från designtill tillverkning av en vindstunnelstödstruktur för en konceptuell UAV av typenflygande vinge, designad av KTH Green Raven Projectstudenter.Den innovativaflygplanskonstruktionen visar hållbarhet inom flygindustrin genom att användahybridbränsleceller som framdrivningssystem. Vindtunneltest som genomförs vidBristol University kommer att producera data för att utvärdera de aerodynamiskaegenskaperna hos modellen för verifiering av designen. Vindtunnelmodellen är ennedskalad modell på 1,5 m som stöds av stag som ändrar anfallsochgirvinklarnaunder testningen. En extern mätsond från Bristol University mäter de krafter ochmoment som modellen utsätts för. De viktigaste kraven för konstruktionen är attmotstå de aerodynamiska lasterna som modellen påför och att ändra modellensorientering samtidigt som vindhastigheten bibehålls under testet. De maximalaaerodynamiska belastningarna tillhandahölls i en matris; varav den största användessom lastfall för stödet motsvarande en 512N lyftkraft vid 14◦ anfallsvinkel. Jämförandestudier genomfördes för att bestämma mekanismerna för att uppfylla kraven samtidigtsom de låg inom budgeten. Den valda konstruktionen för stödkonstruktionenbestår av en cirkulär basplatta som fixeras med hjälp av en låsring, och som harpositioneringsstift för att ändra girvinkeln. En huvudstång är monterad i mitten avbasplattan upp till ett gångjärnsfäste i modellen. Bakom detta sitter ett linjärt ställdonsom dras ut och skjuts ihop för att ändra modellens attityd med rotationscentrum viddet övre fästet på huvudstaget. När designen slutfördes gjordes en finit elementanalysför att verifiera dess strukturella stabilitet. FEAresultatenjämfördes med EulerBernoulliuppskattningarför utböjning. Tillverkningen av komponenterna överlätstill extern part, medan monteringen och programmeringen av ställdonet gjordesinternt.

Photogrammetry is a great technology to check and track deformations on anysurface. This information is critical in many tranportation industries such as aeronautics and the automotive industry. In this thesis report photogrammetry measurements were done using 2 Aicon cameras providing 3D targets coordinates. The goal of this thesis was to ensure the best environment and positioning of the cameras to gather a good amount and quality of data. First positioning of the cameras is optimized by generating a map of the best projected areas that give the best coverage possible of the object. Then all the post processing was done with python using various mathematical methods to extract as much information as possible from the data recorded. First, data transformation to the correct coordinate system was performed using a sparse point-to-plane ICP algorithm. Then missing data was recovered by interpolating it over the time range. Finally raw deflections measurement were extracted and post processed to get essential information such as rigid body motion and static deformation. After an introduction about what is photogrammetry and why it is of high importance in transportation industries, this thesis tackles all the relative challenges that any photogrammetry specialist may face when dealing with such a technology. / Fotogrammetri är en bra teknologi för att kontrollera och spåra deformationer på olika ytor. Denna information är mycket viktig i flera transportindustrier som flyg och fordonsindustrin. I detta examensarbete genomfördes fotogrammetri med två Aicon kameror som ger koordinator för 3D mål. Målet med examensarbetet var att säkerställa så pass bra miljö och positionering av kamerorna som möjligt för att nå bra kvalité på data. Först är positioneringen av kamerorna optimerade genom att generera en karta av de bästa projiserade ytorna som ger den bästa täckningen av objektet. Sedan genomfördes post processing med pyton skript och olika matematiska metoder för att extrahera så mycket information som möjligt från datan. Först genomfördes koordinattransformation till rätt koordinatsystem genom en gles punkt-till-plan ICP algoritm. Sedan återskapades missad data genom interpolation över tid. Slutligen så extraherades deflektioner och post processades för att få viktig information så som stelkroppsrörelser och statisk deformation. Efter en introduktion om vad fotogrammetri är och varför det är viktigt för transportindutrin så tar detta examensarbete upp alla relativa utmaningar som alla fotogrammetriexperter kan tänkas stöta på när det arbetar med denna teknologi.

Highly automated driving is approaching reality at a high speed. BMW is planningto put its first autonomous driving vehicle on the road already by 2021. The path torealising this new technology is however, full of challenges. Not only the transverseand longitudinal dynamic vehicle motion play an important role in experiencedcomfort but also the requirements and expectations of the occupants regarding thevertical dynamic vibration behaviour. Especially during long trips on the motorwaywhere the so far active driver becomes the chauffeured passenger, who reads, worksor sleeps in his newly gained time. These new use-cases create new requirements forthe future design of driving comfort which are yet to be fully discovered.This work was carried out at the BMW headquarters and had the aim to usedifferent machine learning models to investigate and identify patterns between thesubjective comfort values reported by participants in a study, on a comfort scale of 1-7 and the mechanical vibrations that they experienced, measured inm/s2. The datawas collected in a previous independent study and statistical methods were used toinsure the quality of the data. A comparison of the ISO 2631-1 comfort ratings andthe study’s findings is done to understand the need for a more sophisticated model to predict comfort in autonomous driving. The work continued by investigating different dimensionality reduction methods and their influence on the performance of the models. The process used to build, optimise and validate neural networks and other models is included in the method chapter and the results are presented. The work ends with a discussion of both the prediction results and the modelsre-usability. The machine learning models investigated in this thesis have shown great po-tential for detecting complex pattern that link feelings and thoughts to mechanical variables. The models were able to predict the correct level of comfort with up to50% precision when trying to predict 6 or 7 levels of comfort. When divided into high versus low discomfort, i.e. predicting one of two comfort levels, the models were able to achieve a precision of up to 75.4%.Excluded from this thesis is the study of differences in attentive vs inattentive state when being driven in an autonomous driving vehicle. It became clear shortly before the start of this work, that the experiment that yielded the data used for it failed to find a statistically significant difference between the two states. / Självkörande bilar är snart inte längre en dröm utan en mycket sann verklighet. År 2021 planerar BMW att släppa ut sin första autonoma bil på vägarna. Dock är vägen till att förverkliga denna nya teknik full av utmaningar. Utöver den tvärgående och längsgående dynamiska styrningen av fordonet, så spelar även passagerarens förväntningar på det vertikala dynamiska vibrationsbeteendet en växande roll. Speciellt under långa resor på motorvägen där den för nuvarande aktiva föraren blir passagerare, som läser, arbetar eller sover under sin nyvunna tid. De nya användarsenarierna ställer i sin tur nya krav på bilens komfort. Krav som inte har blivit hittills utförligt undersäkta, fastän de kan komma att spela en stor roll i teknikens framgång.Detta examensarbete genomfördes hos BMW:s huvudkontor i Tyskland och hade som mål att undersöka olika maskininlärningsmodeller och deras förmåga att identifiera mönster mellan de subjektiva komfortvärden som rapporterats av deltagarna i en studie, givna på skala 1-7, och de mekaniska vibrationerna som de upplevde mätta i m/s^2. Uppgifterna samlades in i en tidigare oberoende studie. Statistiska metoder användes för att säkerställa datakvaliteten. I detta arbeter har en jämförelse mellan ISO 2631-1-komfortbedömningar och undersökningsresultaten gjorts för att förstå behovet av en mer sofistikerad komfortstandard för att objektifera komfort i självkörande bilar. Arbetet fortsatte med att undersöka olika metoder för att minska datadimensionerna och deras inflytande på modellernas prestanda. Processen som används för att bygga, optimera och validera neurala nätverk och andra modeller är inkluderad i metoddelen och resultaten är presenterade och förklarade därefter. Arbetet avslutas med en diskussion kring både resultatets validitet och modellernas användbarhet.De maskininlärningsmodeller som undersöktes i detta examensarbete har visat stor potential för att upptäcka komplexa mönster som kopplar känslor och tankar till mekaniska variabler. Modellerna kunde förutsäga rätt komfortnivå med upp till 50% precision när 6 eller 7 nivåer av komfort användes. Vid uppdelning i hög mot låg komfort, dvs att kunna förutsäga en av två komfortnivåer, kunde modellerna uppnå en precision på upp till 75.4%.

Planing hull is one solution to break the speed barrier of conventional hull, but as the boat reaches a high speed, massive whisker spray will be developed and attached to the hull, which causes a notable resistance increase. A Swedish company Peterstep invented an innovative spray deflector that can deflect the spray backwards and harvest kinetic energy from the spray.In the 2019 spray deflector project, many tests were done in Davison Laboratory Towing Tank, and there is a trim angle difference between plated and non-plated hulls. To investigate possible reasons, more tests are implemented in this project. According to the test results, the reason is determined as the different roughness of the hull and bottom due to differences in materials. Also, the tape for sealing the seam between hull and bottom plate affects the sharpness of the hard chine, thereby hindering the flow separation.The model used in previous experiments is no longer suitable for the further investigation. The modular design caused the different running position of plated and non-plated hull. In addition, the hull is too slender for the wave test. Therefore, a new model is needed to satisfy the new objectives of experiments. In this paper, the detailed design is surrounded by design aims and restrictions, such as increase spray resistance and avoid porpoising.There are few researches on HSC free running model test. To investigate the performance of the spray deflector in the test environment more similar to reality, a free running model with propulsion and steering system is necessary. The preliminary design, component selection and testing plan are outlined in this paper. / Planande skrov är en lösning för att bryta hastighetsbarriären hos ett konventionellt skrov, men när båten når hög hastighet kommer omfattande whisker spray att utvecklas på skrovet, vilket orsakar en anmärkningsvärd ökning av motståndet. Ett svenskt företag Peterstep har utvecklat en innovativ sprutdeflektor som kan avleda sprayen bakåt och skörda kinetisk energi från sprayen.Under sprutdeflektorprojektet 2019 gjordes många tester i Davison Laboratorys släpränna och det noterades en oönskad trimvinkelskillnad mellan modeller där skrovet byggts i en del eller med ett steg som fyllts igen med en bottenplatta. För att undersöka möjliga skäl till detta implementeras nya tester i detta projekt. Enligt testresultaten bestäms orsaken som skrovets och bottenplattans olika jämnhet på grund av materialskillnader. Även tejpen för tätning av sömmen mellan skrov och bottenplatta påverkar skärpan i slaget och hindrar därmed flödets avlösning.Modellen som använts i tidigare experiment är inte lämplig för fortsatt utredningen. Den modulära designen orsakade olika gångläge beroende på hur skroven hade byggts upp. Dessutom är skrovet för smalt för vågproven. Det behövs därför en ny modell för att uppfylla målen med experimenten.I det här arbetet har designen ytterligare designmål och begränsningar, som att mäta sprutmotståndet och att undvika porpoising.Det finns få undersökningar om HSC-test med frigående modeller. För att undersöka sprutdeflektorers prestanda i testmiljö som liknar verkligheten är det nödvändigt med en frigående modell med eget framdrivnings- och styrsystem. Den preliminära designen, komponentvalet och testplanen beskrivs i detta dokument.

Optimization methods are commonly used to develop new products and are also an importantstep in more incremental design improvements. In the maritime industry, these methodsare often used to create more ecient vessels and to ful ll the environmental requirementsimposed by the IMO. In recent years, the adjoint method have been used more frequently.This method can be used to predict the inuence of some input parameters on a quantityin a Computational Fluid Dynamics (CFD) simulation.In this project, the adjoint method has been investigated and applied on a relevant case;how it can be used to reduce the drag of a twisted rudder by changing the twist angles.STAR-CCM+ has been used to perform the CFD and adjoint simulations. These resultshave been imported to CAESES, a CAD-modeler, which connects the adjoint results to thedesign parameters. The adjoint results indicate a possible change of the design parameter,the twist angle is modi ed based on these results and a new geometry of the rudder is constructedin CAESES. Furthermore, the numerical results indicates that the method can beused to reduce the drag on the rudder. One of the cases in the project achieved a reductionof the rudder drag by 3.35 % and the total drag decreased with 0.18 %. However, the othertwo cases did not achieve a reduction of the drag and hence further investigations needs tobe done.The adjoint method have the possibility to be a good optimization alternative for developmentof new products or in engineering-to-order processes. The option of connecting theadjoint results to design parameters is a great advantage. On the other hand, the method inthis project is not reliable and the reason for the contradictory results needs to be studiedfurther. / Optimeringsmetoder är vanligt förekommande när nya produkter utvecklas och är också ett viktigt steg i inkrementella designförbättringar. I sjöfartsindustrin används dessa metoder för att skapa effektivare fartyg och för att uppfylla miljökraven framtagna av IMO. På senare år har adjointmetoden börjat användas mer. Metoden kan användas för att förutspåindataparametrars inverkan på en kvantitet i en strömningsmekanisk beräkning, även kallat CFD. I det här projektet ska adjointmetoden utvärderas och hur den kan användas för att reducera motståndet på ett tvistat roder genom att ändra tvist vinklarna. STAR-CCM+ har använts för att utföra CFD- och adjointberäkningarna. Dessa resultat importerades till en CAD-modellerare, CAESES, som kopplar adjointresultaten till designvariabler. Resultaten från adjointsimuleringen indikerar en möjlig förändring av designvariabeln, som sedan ändras utefter detta resultat och en ny rodergeometri genereras av CAESES. De numeriska resultaten indikerar att adjointmetoden kan användas för att reducera motståndet på ett tvistat roder. I ett av fallen i projektet reducerades motståndet med 3,35 % och det totala motståndet för hela fartyget reducerades med 0,18 %. Däremot så påvisade två andra fall ingen förändring av rodermotståndet och anledningen till detta kräver ytterligare unders ökningar. Adjointmetoden har möjligheterna att bli ett bra alternativ i en optimeringsprocess och för utveckling av nya produkter. Möjligheten att koppla adjointresultaten till designvariabler är också en stor fördel. Däremot så är metoden i detta projekt inte så tillförlitlig och anledningen till de motsägelsefulla resultaten måste studeras ytterligare.