Log in

Relevant bibliographies by topics / Aerospace Structure / Dissertations / Theses

To see the other types of publications on this topic, follow the link: Aerospace Structure.

Dissertations / Theses on the topic 'Aerospace Structure'

Author: Grafiati

Published: 14 March 2023

Last updated: 31 July 2025

Create a spot-on reference in APA, MLA, Chicago, Harvard, and other styles

Select a source type:

Consult the top 50 dissertations / theses for your research on the topic 'Aerospace Structure.'

Next to every source in the list of references, there is an 'Add to bibliography' button. Press on it, and we will generate automatically the bibliographic reference to the chosen work in the citation style you need: APA, MLA, Harvard, Chicago, Vancouver, etc.

You can also download the full text of the academic publication as pdf and read online its abstract whenever available in the metadata.

Browse dissertations / theses on a wide variety of disciplines and organise your bibliography correctly.

1

Ahn, Junghyun. "Integrated analysis procedure of aerospace composite structure." Thesis, Massachusetts Institute of Technology, 2008. http://hdl.handle.net/1721.1/43106.

Full text

Abstract:

Thesis (S.M.)--Massachusetts Institute of Technology, System Design and Management Program, 2008.<br>Includes bibliographical references (p. 50).<br>The emergence of composite material application in major commercial aircraft design, represented by the Boeing 787 and Airbus A350-XWB, signals a new era in the aerospace industry. The high stiffness to weight ratio of continuous fiber composites (CFC) makes CFCs one of the most important materials to be introduced in modern aircraft industry. In addition to inherent strength (per given weight) of CFCs, they also offer the unusual opportunity to d

APA, Harvard, Vancouver, ISO, and other styles

2

Key, Ross A. "Automated manufacturing processes for secondary structure aerospace composites." Thesis, University of Nottingham, 2016. http://eprints.nottingham.ac.uk/33572/.

Full text

Abstract:

As projected manufacturing rates for commercial aircraft increase to levels of multiple ship sets per day from individual manufacturing facilities, GE Aviation have expressed the need for a shift in composites secondary structure manufacturing philosophy. Traditional manufacturing processes tend to be touch labour intensive and hence costly. The manual placement of large numbers of individual ply profiles, lengthy debulking operations and complex cure cycles, result in excessive component lead times and manufacturing costs. As a result, direct labour cost is a major factor in the total economi

APA, Harvard, Vancouver, ISO, and other styles

3

Hu, Zhuopei. "Finite Element Modeling of Aerospace Materials and Structure." University of Akron / OhioLINK, 2012. http://rave.ohiolink.edu/etdc/view?acc_num=akron1344224158.

Full text

APA, Harvard, Vancouver, ISO, and other styles

4

Zheng, LiangKan 1972. "Fluid-structure coupling for aeroelastic computations in the time domain using low fidelity structural models." Thesis, McGill University, 2005. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=99127.

Full text

Abstract:

Flutter analysis plays an important role in the design and development of aircraft wings because of the information it provides regarding the flight envelope of the aircraft. With the coupling of the flow and structural solver, the flutter boundary of wings can be evaluated in the time domain. This study: First, computes the aeroelastic response for a typical sweptback wing section model by coupling a flow solver and a two degree of freedom structural equation of motion solver to predict the flutter boundary of an airfoil at different Mach numbers. The results agree well with previous numerica

APA, Harvard, Vancouver, ISO, and other styles

5

Seddon, Caroline Michelle. "Modelling transient dynamic fluid-structure interaction in aerospace applications." Thesis, University of Salford, 2006. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.492434.

Full text

Abstract:

Although significant progress has been made in the study of dynamic loading of aircraft structures, several areas have been identified that require further research. In particular, attention is drawn to problems involving transient, dynamic fluid-structure interaction, where fluids play an important role, heavily influencing the response of the structure to the applied dynamic load. In this work the use of existing numerical modelling techniques for the evaluation of such problems is investigated.

APA, Harvard, Vancouver, ISO, and other styles

6

Bhatti, Wasim. "Mechanical integration of a PEM fuel cell for a multifunctional aerospace structure." Thesis, Loughborough University, 2016. https://dspace.lboro.ac.uk/2134/21513.

Full text

Abstract:

A multifunctional structural polymer electrolyte membrane (PEM) fuel cell was designed, developed and manufactured. The structural fuel cell was designed to represent the rear rib section of an aircraft wing. Custom membrane electrode assemblies (MEA s) were manufactured in house. Each MEA had an active area of 25cm2.The platinum loading on each electrode (anode and cathode) was 0.5mg/cm2. Sandwiched between the electrodes was a Nafion 212 electrolyte membrane. Additional components of the structural fuel included metallic bipolar plates and end plates. Initially all the components were manufa

APA, Harvard, Vancouver, ISO, and other styles

7

Palsule, Sanjay. "Structure and properties of aerospace molecular composites : third generation polymers." Thesis, Heriot-Watt University, 1994. http://hdl.handle.net/10399/1388.

Full text

APA, Harvard, Vancouver, ISO, and other styles

8

Khataee, Amin. "Structure and properties of some Ti-Al-Ru alloys." Thesis, Imperial College London, 1987. http://hdl.handle.net/10044/1/46915.

Full text

APA, Harvard, Vancouver, ISO, and other styles

9

Liang, Lijun. "Experimental investigation of an aeroelastic structure with continuous nonlinear stiffness." Thesis, McGill University, 2003. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=80123.

Full text

Abstract:

An experimental investigation is presented for the aeroelastic response of a two-degree-of-freedom airfoil positioned in an incompressible flow. In particular, the effects of cubic structural nonlinearities in the pitch degree-of-freedom are considered. These nonlinearities are introduced via a specially designed pitch cam, which permits different degrees of nonlinearity, as well as a linear system, to be obtained.<br>Several linear and nonlinear system tests are presented, and the results compared and analyzed. The effects of linear plunge stiffness on the stability of the aeroelastic

APA, Harvard, Vancouver, ISO, and other styles

10

Ozsoy, Serhan. "Vibration Induced Stress And Accelerated Life Analyses Of An Aerospace Structure." Master's thesis, METU, 2006. http://etd.lib.metu.edu.tr/upload/2/12606966/index.pdf.

Full text

Abstract:

Fatigue failure of metallic structures operating under dynamic loading is a common occurrence in engineering applications. It is difficult to estimate the response of complicated systems analytically, due to structure&amp<br>#8217<br>s dynamic characteristics and varying loadings. Therefore, experimental, numerical or a combination of both methods are used for fatigue evaluations. Fatigue failure can occur on systems and platforms as well as components to be mounted on the platform. In this thesis, a helicopter&amp<br>#8217<br>s Missile Warning Sensor - Cowling assembly is analyzed. Analytical

APA, Harvard, Vancouver, ISO, and other styles

11

Beji, Faycel Ben Hedi. "Buckling Analysis of Composite Stiffened Panels and Shells in Aerospace Structure." Thesis, Virginia Tech, 2018. http://hdl.handle.net/10919/81620.

Full text

Abstract:

Stiffeners attached to composite panels and shells may significantly increase the overall buckling load of the resultant stiffened structure. Initially, an extensive literature review was conducted over the past ten years of published work wherein research was conducted on grid stiffened composite structures and stiffened panels, due to their applications in weight sensitive structures. Failure modes identified in the literature had been addressed and divided into a few categories including: buckling of the skin between stiffeners, stiffener crippling and overall buckling. Different methods ha

APA, Harvard, Vancouver, ISO, and other styles

12

Vestlund, Oscar. "Aerodynamics and Structure of a Large UAV." Thesis, Mälardalens högskola, Akademin för innovation, design och teknik, 2018. http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-38562.

Full text

Abstract:

This thesis investigates what design of a large UAV performing VTOL using only electrical motors is the most viable in terms of extending its range. Because it uses batteries for power, its powered time is limited, posing the need for a way of extending its flight time. By using a tiltwing design, its vertical flight time is cut at the same time as it will be able to perform as a glider, increasing its range drastically. To achieve the best lift-to-drag ratio, the high-lift F3B RG15-airfoil was chosen, giving the UAV a lift-to-drag ratio of 36,48, and a maximum range per descend glide of appro

APA, Harvard, Vancouver, ISO, and other styles

13

Bingham, Christopher Malcolm. "Application of variable structure control methods to actuator nonlinearities in aerospace systems." Thesis, Cranfield University, 1994. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.358823.

Full text

APA, Harvard, Vancouver, ISO, and other styles

14

Roy, Steven. "Mechanical modeling and testing of a composite helicopter structure made by resin transfer moulding." Thesis, McGill University, 2009. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=40829.

Full text

Abstract:

The design and mechanical performance of a helicopter horizontal stabilizer slat made by resin transfer moulding (RTM) can be evaluated with finite element analysis (FEA). To verify the validity of the assumptions used in the modelling of the slat structure, static mechanical tests were performed on prototype slats which were half of the full-size length. The slat complex boundary conditions were simplified to make static mechanical testing possible. Two fixtures were designed and built to introduce simplified loads in specimens with two different bracket configurations: a full and a half brac

APA, Harvard, Vancouver, ISO, and other styles

15

Farinha, Marques Vitor Manuel. "Lead free solders for aerospace applications." Thesis, University of Oxford, 2010. http://ora.ox.ac.uk/objects/uuid:85707054-bc46-44f3-b9c6-9fd29358ad25.

Full text

Abstract:

The factors controlling the reliability of Pb-free solders when subject to thermomechanical regimes relevant to the harsh aerospace environment have been studied. Ball grid array (BGAs) typical of microelectronic devices have been manufactured in-house and subjected to isothermal ageing and thermal cycling. The BGAs comprised both Cu and Ni-Au metallizations, Pb-free Sn-Ag-Cu 400 and 600μm solder balls, FR4 and Al<sub>2</sub>O<sub>3</sub> boards, and included circuits to measure resistance changes due to damage in the joints during thermal cycling. Microstructural evolution within the solde

APA, Harvard, Vancouver, ISO, and other styles

16

Fry, Zachary S. "A LABORATORY SCALE STUDY OF INTUMESCENT COATINGS FOR PROTECTION OF BUILDING STRUCTURE MEMBERS FROM FIRES." Case Western Reserve University School of Graduate Studies / OhioLINK, 2014. http://rave.ohiolink.edu/etdc/view?acc_num=case1402055149.

Full text

APA, Harvard, Vancouver, ISO, and other styles

17

Holder, Justin. "Fluid Structure Interaction in Compressible Flows." University of Cincinnati / OhioLINK, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=ucin159584692691518.

Full text

APA, Harvard, Vancouver, ISO, and other styles

18

Vishwakarma, R. "The use of inverse methods in determining applied dynamic loads on aerospace structure." Thesis, University of Hertfordshire, 2012. https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.691048.

Full text

APA, Harvard, Vancouver, ISO, and other styles

19

CERRACCHIO, PRISCILLA. "Inverse methods for health monitoring and shape sensing of aerospace structures." Doctoral thesis, Politecnico di Torino, 2014. http://hdl.handle.net/11583/2538725.

Full text

Abstract:

Shape sensing, i.e., reconstruction of the displacement field of a structure from surface-measured strains, has relevant implications for Structural Health Monitoring (SHM), as well as for control and actuation of smart structures. The knowledge of the full-field displacements implies that other essential response quantities such as stresses can be assessed, thus enabling real-time damage predictions by means of appropriate failure criteria. The inverse Finite Element Method (iFEM) is a shape-sensing methodology shown to be fast, accurate, and robust. In the present thesis, the general framewo

APA, Harvard, Vancouver, ISO, and other styles

20

Park, Conrad. "Mechanical Performance and Structure-Property Relations in6061B Aluminum Metal Matrix Composites." Case Western Reserve University School of Graduate Studies / OhioLINK, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=case1547842396716777.

Full text

APA, Harvard, Vancouver, ISO, and other styles

21

Drury, William David. "An adaptive structure based sensorless position estimator for permanent magnet machines in aerospace applications." Thesis, University of Bristol, 2010. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.654114.

Full text

Abstract:

The application of the research is towards brushless ac permanent magnet machine drives of the type deployed in aerospace actuation systems. These drives tend to utilise motor designs having concentrated windings with a low slot to pole ratio and thus are not ideal sinusoidal machines. In addition, these machines are often required to operate both below base speed and in the field-weakened region. The proposed sensorless technique, based on two flux models, avoids the need for differentiation in the position and speed estimation, is computationally efficient and is robust to temperature depend

APA, Harvard, Vancouver, ISO, and other styles

22

Korobenko, Artem. "Advanced Fluid--Structure Interaction Techniques in Application to Horizontal and Vertical Axis Wind Turbines." Thesis, University of California, San Diego, 2015. http://pqdtopen.proquest.com/#viewpdf?dispub=3670451.

Full text

Abstract:

<p> During the last several decades engineers and scientists put significant effort into developing reliable and efficient wind turbines. As a wind power production demands grow, the wind energy research and development need to be enhanced with high-precision methods and tools. These include time-dependent, full-scale, complex-geometry advanced computational simulations at large-scale. Those, computational analysis of wind turbines, including fluid-structure interaction simulations (FSI) at full scale is important for accurate and reliable modeling, as well as blade failure prediction and desi

APA, Harvard, Vancouver, ISO, and other styles

23

Bail, Justin L. "Non-desctructive investigation & FEA correlation on an aircraft sandwich composite structure." Akron, OH : University of Akron, 2007. http://rave.ohiolink.edu/etdc/view?acc%5Fnum=akron1196702586.

Full text

Abstract:

Thesis (M.S.)--University of Akron, Dept. of Civil Engineering, 2007.<br>"December, 2007." Title from electronic thesis title page (viewed 02/25/2008) Advisor, Wieslaw Binienda; Faculty readers, Craig Menzemer, Robert Goldbert; Department Chair, Wieslaw Binienda; Dean of the College, George K. Haritos; Dean of the Graduate School, George R. Newkome. Includes bibliographical references.

APA, Harvard, Vancouver, ISO, and other styles

24

Bin, Abdullah Nur Azam. "Numerical modelling and interaction of crack and aeroelastic behaviour of composite structure for aerospace applications." Thesis, University of Sheffield, 2018. http://etheses.whiterose.ac.uk/21462/.

Full text

Abstract:

Aeroelasticity and fracture mechanics are two fields that commonly known will result in a structural failure. However, small attention is given in assessing the structural integrity of any flying object in aerospace application subjected to aerodynamic or aeroelastic loads especially the aircraft wing. The current research in the aircraft industry is focusing on the development of advanced composite wing structure, which there are still not well explored widely. Due to the higher strength of composite materials, a stronger wing could be designed to sustain the aerodynamic loads or any gust tur

APA, Harvard, Vancouver, ISO, and other styles

25

Michaels, Simone Colette. "Development and Assessment of Artificial Manduca sexta Forewings: How Wing Structure Affects Performance." Case Western Reserve University School of Graduate Studies / OhioLINK, 2016. http://rave.ohiolink.edu/etdc/view?acc_num=case1446206590.

Full text

APA, Harvard, Vancouver, ISO, and other styles

26

He, Yunzheng. "Modeling and Simulation of Tensegrity Structure based on SimMechanics." University of Cincinnati / OhioLINK, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1592395403390476.

Full text

APA, Harvard, Vancouver, ISO, and other styles

27

Puttmann, John Paul. "Spatially Targeted Activation of a SMP." University of Dayton / OhioLINK, 2018. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1525166147319011.

Full text

APA, Harvard, Vancouver, ISO, and other styles

28

Hinton, David A. "The organization as a system : structure, process, and human capital considerations in aerospace R&T." Thesis, Massachusetts Institute of Technology, 2003. http://hdl.handle.net/1721.1/91790.

Full text

APA, Harvard, Vancouver, ISO, and other styles

29

Inman, Jennifer Ann. "Fluorescence imaging study of free and impinging supersonic jets: Jet structure and turbulent transition." W&M ScholarWorks, 2007. https://scholarworks.wm.edu/etd/1539623513.

Full text

Abstract:

A series of experiments into the behavior of underexpanded jet flows has been conducted at NASA Langley Research Center. This work was conducted in support of the Return to Flight effort following the loss of the Columbia. The tests involved simulating flow through a hypothetical breach in the leading edge of the Space Shuttle Orbiter along its reentry trajectory, with the goal of generating a data set with which other researchers can test and validate computational modeling tools. Two nozzles supplied with high-pressure gas were used to generate axisymmetric underexpanded jets exhausting into

APA, Harvard, Vancouver, ISO, and other styles

30

Nwankpa, Uzoma Vincent. "Effectiveness of arc based processes and deposition strategies on additive manufacture structure for naval and aerospace applications." Thesis, Ecole centrale de Nantes, 2022. http://www.theses.fr/2022ECDN0010.

Full text

Abstract:

Le processus de fabrication additive par fusion de fil métallique par arc électrique (Wire Arc Additive Manufacturing, WAAM) est devenu un procédé pertinent pour la fabrication de composants de structures complexes, qui étaient très compliqués à réaliser avec les méthodes de fabrication conventionnelles. Différents procédés à base d'arc électriques sont disponibles pour la mise en œuvre de matériaux tels que les alliages de titane ou d'aluminium et les aciers inoxydables, afin de produire des composants de grandes tailles. Néanmoins, il reste à déterminer quel est le meilleur procédé à base d'

APA, Harvard, Vancouver, ISO, and other styles

31

Chamberlain, Britany L. "Additively-Manufactured Hybrid Rocket Consumable Structure for CubeSat Propulsion." DigitalCommons@USU, 2018. https://digitalcommons.usu.edu/etd/7285.

Full text

Abstract:

Three-dimensional, additive printing has emerged as an exciting new technology for the design and manufacture of small spacecraft systems. Using 3-D printed thermoplastic materials, hybrid rocket fuel grains can be printed with nearly any cross-sectional shape, and embedded cavities are easily achieved. Applying this technology to print fuel materials directly into a CubeSat frame results in an efficient, cost-effective alternative to existing CubeSat propulsion systems. Different 3-D printed materials and geometries were evaluated for their performance as propellants and as structural element

APA, Harvard, Vancouver, ISO, and other styles

32

Mignee, Juliette L. "Proper Orthogonal Decomposition Applied to a Supersonic Single Flow Jet." University of Cincinnati / OhioLINK, 2012. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1329935384.

Full text

APA, Harvard, Vancouver, ISO, and other styles

33

Khasawneh, Firas Abdallah. "Characterization of drillability of sandwich structure of carbon fiber reinforced epoxy composite over titanium alloy." Diss., Columbia, Mo. : University of Missouri-Columbia, 2006. http://hdl.handle.net/10355/5871.

Full text

Abstract:

Thesis (M.S.)--University of Missouri-Columbia, 2006.<br>The entire dissertation/thesis text is included in the research.pdf file; the official abstract appears in the short.pdf file (which also appears in the research.pdf); a non-technical general description, or public abstract, appears in the public.pdf file. Title from title screen of research.pdf file (viewed on September 13, 2007). Vita. Includes bibliographical references.

APA, Harvard, Vancouver, ISO, and other styles

34

DE, LA PIERRE DES AMBROIS STEFANO. "Advanced joined materials development and their shear strength evaluation for aerospace, energy and structural applications." Doctoral thesis, Politecnico di Torino, 2020. http://hdl.handle.net/11583/2845790.

Full text

APA, Harvard, Vancouver, ISO, and other styles

35

Bail, Justin. "Non-Destructive Investigation & FEA Correlation on an Aircraft Sandwich Composite STructure." University of Akron / OhioLINK, 2007. http://rave.ohiolink.edu/etdc/view?acc_num=akron1196702586.

Full text

APA, Harvard, Vancouver, ISO, and other styles

36

Brod, Stephen P. 1970. "A testbed for investigating the effect of electrode structure on the performance of a solid oxide electrolysis system." Thesis, The University of Arizona, 1995. http://hdl.handle.net/10150/291547.

Full text

Abstract:

In-Situ Resource Utilization (ISRU) can reduce the mass launched to low Earth orbit for a Mars Sample Return Mission by as much as 75%. Solid Oxide Electrolysis is a candidate technology for producing oxygen out of carbon dioxide. A testbed was developed to test the effect of electrode structure on electrode performance. The testbed used all metal interconnects. Electrodes of 0.5 microns (applied by evaporative deposition) and 10-12 microns thick (applied by airbrushing) were produced. The disks were tested in argon, oxygen, and carbon dioxide. The thin electrode showed deterioration in both s

APA, Harvard, Vancouver, ISO, and other styles

37

BOLLINO, ARCANGELA. "QUASI STATIC GRAVITY SIGNATURES IN SLOW TECTONIC ZONES: ASSIMILATION OF NOVEL AEROSPACE DATA AND GEOPHYSICAL MODELING." Doctoral thesis, Università degli Studi di Milano, 2023. https://hdl.handle.net/2434/956505.

Full text

Abstract:

The main aim of my Ph.D. research project was to investigate the gravitational signatures of the mechanisms that regulate slow rate tectonic deformation in areas where the earthquakes enucleate. 2D thermo-mechanical numerical models are used to simulate the crust-mantle dynamics; in particular, complexities such as compositional stratification of crust-lithosphere system, mantle hydration, phase changes and degree of plate coupling are investigated, exploring how they affect the gravity field and its rate of change in different tectonic environments. A strongly integration between modelling,

APA, Harvard, Vancouver, ISO, and other styles

38

Witeof, Zachary. "Exploratory Study on the Design of Combined Aero-Thermo-Structural Experiments in High Speed Flows." The Ohio State University, 2013. http://rave.ohiolink.edu/etdc/view?acc_num=osu1366213825.

Full text

APA, Harvard, Vancouver, ISO, and other styles

39

Rinehart, Aidan Walker. "A Characterization of Seal Whisker Morphology and the Effects of Angle of Incidence on Wake Structure." Cleveland State University / OhioLINK, 2016. http://rave.ohiolink.edu/etdc/view?acc_num=csu1483991011265196.

Full text

APA, Harvard, Vancouver, ISO, and other styles

40

Miller, Samuel C. "Fluid-Structure Interaction of a Variable Camber Compliant Wing." University of Dayton / OhioLINK, 2015. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1428575972.

Full text

APA, Harvard, Vancouver, ISO, and other styles

41

Magal, Rithvik. "Development and validation of a mathematical model for a monotube automotive damper." Master's thesis, Alma Mater Studiorum - Università di Bologna, 2021. http://amslaurea.unibo.it/22951/.

Full text

Abstract:

Automotive dampers involve complex flow physics that cannot be fully described by analytical models derived from first principles. Therefore, the development of a mathematical model based on semi-empirical laws that accurately describe the influence of each of the many design features would greatly help the design and optimization of automotive dampers. This thesis aims to develop a computationally efficient mathematical model capable to predicting damper performance with reasonable accuracy. Lumped parameter mathematical models were developed and implemented using the MATLAB and Simulink env

APA, Harvard, Vancouver, ISO, and other styles

42

Byrd, Alex W. "Fluid-Structure Interaction Simulations of a Flapping Wing Micro Air Vehicle." Wright State University / OhioLINK, 2014. http://rave.ohiolink.edu/etdc/view?acc_num=wright1401559891.

Full text

APA, Harvard, Vancouver, ISO, and other styles

43

Hart, Peter Bartholomew. "A plm implementation for aerospace systems engineering-conceptual rotorcraft design." Thesis, Georgia Institute of Technology, 2009. http://hdl.handle.net/1853/28278.

Full text

Abstract:

The thesis will discuss the Systems Engineering phase of an original Conceptual Design Engineering Methodology for Aerospace Engineering-Vehicle Synthesis. This iterative phase is shown to benefit from digitization of Integrated Product&Process Design (IPPD) activities, through the application of Product Lifecycle Management (PLM) technologies. Requirements analysis through the use of Quality Function Deployment (QFD) and 7 MaP tools is explored as an illustration. A "Requirements Data Manager" (RDM) is used to show the ability to reduce the time and cost to design for both new and legacy/deri

APA, Harvard, Vancouver, ISO, and other styles

44

Fernández, Bravo Elena. "Modelling and testing of a solar panel structure for KNATTE (Kinesthetic Node and Autonomous Table-Top Emulator)." Thesis, Luleå tekniska universitet, Institutionen för system- och rymdteknik, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-87200.

Full text

Abstract:

One of the challenges that satellites face is the interaction between control movement and vibration of flexible appendages such as solar arrays and antennas that can negatively affect the performance of the spacecraft. The aim of this thesis is to develop a numerical model of a solar panel structure for KNATTE, a frictionless platform developed by the Onboard Space Systems group at Luleå University of Technology, and develop a control law that reduces the flexible vibration of the solar arrays when attitude control manoeuvres are performed. A set of solar panel structures have been designed a

APA, Harvard, Vancouver, ISO, and other styles

45

Mikol, Collin Everett. "Design, Modeling, and Experimental Testing of a Variable Stiffness Structure for Shape Morphing." The Ohio State University, 2018. http://rave.ohiolink.edu/etdc/view?acc_num=osu1523454926569658.

Full text

APA, Harvard, Vancouver, ISO, and other styles

46

Mills, Austin Shelley. "The Structural Suitability of Tensegrity Aircraft Wings." University of Dayton / OhioLINK, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1590172090108379.

Full text

APA, Harvard, Vancouver, ISO, and other styles

47

Knöös, Franzén Ludvig, and Erik Magnusson. "Weight Penalty Methods for Conceptual Aircraft Design." Thesis, Linköpings universitet, Fluida och mekatroniska system, 2018. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-175012.

Full text

Abstract:

This report addresses a project conducted at Saab Aeronautics during the spring of 2018. The goal of the project was to investigate aircraft weight estimations in the conceptual design phase. The work was divided into two major parts: finding new weight estimation techniques and implementing an existing technique called the Berry Weight Estimation in to the Pacelab APD software. Several weight estimation techniques were found during an extensive literature review but in the end, only one was chosen for further investigation. The chosen technique was the NASA Wing Weight Build-Up which proposed

APA, Harvard, Vancouver, ISO, and other styles

48

Pesich, Justin M. "Steady Aeroelastic Response Prediction and Validation for Automobile Hoods." The Ohio State University, 2017. http://rave.ohiolink.edu/etdc/view?acc_num=osu1482329426783128.

Full text

APA, Harvard, Vancouver, ISO, and other styles

49

Wilmoth, Nathan G. "Determining the Mechanical Properties of Lattice Block Structures." Cleveland State University / OhioLINK, 2013. http://rave.ohiolink.edu/etdc/view?acc_num=csu1366275566.

Full text

APA, Harvard, Vancouver, ISO, and other styles

50

Reilly, Daniel Oliver. "Inlet Distortion Effects on the Unsteady Aerodynamics of a Transonic Fan Stage." Wright State University / OhioLINK, 2016. http://rave.ohiolink.edu/etdc/view?acc_num=wright1482139741887976.

Full text

APA, Harvard, Vancouver, ISO, and other styles

We offer discounts on all premium plans for authors whose works are included in thematic literature selections. Contact us to get a unique promo code!