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Relevant bibliographies by topics / Airplanes Aerodynamics / Dissertations / Theses

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Dissertations / Theses on the topic 'Airplanes Aerodynamics'

Author: Grafiati

Published: 4 June 2021

Last updated: 8 February 2022

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1

Zamboni, Giulio. "Fan root aerodynamics." Thesis, University of Cambridge, 2009. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.611841.

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2

Detwiler, Kevin P. "Reduced fan noise radiation from a supersonic inlet." Thesis, This resource online, 1993. http://scholar.lib.vt.edu/theses/available/etd-09192009-040457/.

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3

Fleming, Jonathan Lee. "An experimental study of a turbulent wing-body junction and wake flow." Thesis, This resource online, 1991. http://scholar.lib.vt.edu/theses/available/etd-08222009-040300/.

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4

Wolfe, Douglas E. "Airplane dynamic modeling and automatic flight control design." Master's thesis, This resource online, 1990. http://scholar.lib.vt.edu/theses/available/etd-01202010-020132/.

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5

Mazza, Joseph R. "An experimental and computational aerodynamic investigation of a low-canard high-wing aircraft design." Thesis, This resource online, 1993. http://scholar.lib.vt.edu/theses/available/etd-03172010-020720/.

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6

Peterson, Kevin G. "Rolling moments and aerodynamic time scales for a model with a moving nose stagnation point." Thesis, Georgia Institute of Technology, 1996. http://hdl.handle.net/1853/12048.

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7

Chiu, Yih-wan Danny. "Convergence of discrete-vortex induced-flow calculations by optimum choice of mesh." Diss., Georgia Institute of Technology, 1988. http://hdl.handle.net/1853/12390.

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8

Hazarika, Neep. "An inverse method for blended wing-body configurations." Diss., Georgia Institute of Technology, 1988. http://hdl.handle.net/1853/12498.

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9

Worley, John C. Ahmed Anwar. "Yaw-roll coupled oscillations of a slender delta wing." Auburn, Ala, 2008. http://repo.lib.auburn.edu/EtdRoot/2008/SUMMER/Aerospace_Engineering/Thesis/Worley_John_37.pdf.

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10

Yu, Chao. "An acoustic intensity-based method and its aeroacoustic applications." Diss., Connect to online resource - MSU authorized users, 2008.

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11

Grieshaber, Michele Marie. "Interactive calculation of cross-sectional areas for aircraft design and analysis." Thesis, This resource online, 1988. http://scholar.lib.vt.edu/theses/available/etd-04272010-020357/.

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12

Rysdyk, Rolf T. "Adaptive nonlinear flight control." Diss., Georgia Institute of Technology, 1998. http://hdl.handle.net/1853/12108.

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13

Unger, Eric Robert. "Integrated aerodynamic-structural wing design optimization." Diss., This resource online, 1992. http://scholar.lib.vt.edu/theses/available/etd-09042008-063104/.

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14

Bowersox, Rodney Dale Welch. "Meanflow and turbulence measurements in the wake of a supersonic through-flow cascade." Thesis, This resource online, 1990. http://scholar.lib.vt.edu/theses/available/etd-03122009-040531/.

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15

Darden, Leigh-Ann. "Rolling moment response of a wing-body to stagnation point actuation." Diss., Georgia Institute of Technology, 1997. http://hdl.handle.net/1853/12481.

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16

Kim, ChangEun. "Static and dynamic aeroelastic simulation of wings with state space aerodynamic models." Thesis, Georgia Institute of Technology, 2000. http://hdl.handle.net/1853/12898.

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17

Schuster, D. M. (David M. ). "Application of an aeroelastic analysis method for aerodynamic improvement of fighter wings at maneuver flight conditions." Diss., Georgia Institute of Technology, 1992. http://hdl.handle.net/1853/12367.

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18

Levis, William R. "Unsteady casewall pressure measurements in a transonic compressor during steam induced stall." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2006. http://library.nps.navy.mil/uhtbin/hyperion/06Jun%5FLevis.pdf.

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19

Srigrarom, Sutthiphong. "On the formation of vortex breakdown over delta wings /." Thesis, Connect to this title online; UW restricted, 2001. http://hdl.handle.net/1773/10004.

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20

Wee, Teik Khoo. "Cold flow drag measurement and numerical performance prediction of a miniature ramjet at Mach 4." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2003. http://library.nps.navy.mil/uhtbin/hyperion-image/03Dec%5FWee.pdf.

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Thesis (M.S. in Engineering Science (Mechanical Engineering))--Naval Postgraduate School, December 2003.<br>Thesis advisor(s): Garth V. Hobson, Rayomnd P. Shreeve. Includes bibliographical references (p. 67). Also available online.

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21

Ames, Richard Gene. "On the flowfield and forces generated by a rectangular wing undergoing moderate reduced frequency flapping at low reynolds number." Diss., Georgia Institute of Technology, 2001. http://hdl.handle.net/1853/12468.

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22

Pino, Romainville Francisco Adolfo. "The effect of adding multiple triangular vortex generators on the leading edge of a wing." Morgantown, W. Va. : [West Virginia University Libraries], 2005. https://eidr.wvu.edu/etd/documentdata.eTD?documentid=4405.

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Thesis (M.S.)--West Virginia University, 2005.<br>Title from document title page. Document formatted into pages; contains xiv, 86 p. : ill. (some col.). Includes abstract. Includes bibliographical references (p. 73-76).

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23

Jimeno, Jesus. "A physics based robust methodology for aerodynamic design analysis and optimization." Thesis, Georgia Institute of Technology, 2000. http://hdl.handle.net/1853/12472.

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24

Rohl, Peter Jurgen. "A multilevel decomposition procedure for the preliminary wing design of a high-speed civil transport aircraft." Diss., Georgia Institute of Technology, 1995. http://hdl.handle.net/1853/11827.

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25

Lim, Mun Hong. "Flutter suppression of an unswept wing using acceleration feedback control." Thesis, Georgia Institute of Technology, 1999. http://hdl.handle.net/1853/11983.

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26

Riaz, Jamshed. "A simulation model of atmospheric turbulence for rotorcraft applications." Diss., Georgia Institute of Technology, 1992. http://hdl.handle.net/1853/12940.

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27

Scharl, Julien. "Formulation and implementation of a methodology for dynamic modeling and simulation in early aerospace design." Diss., Georgia Institute of Technology, 2001. http://hdl.handle.net/1853/12973.

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28

Arledge, Thomas K. "ACSYNT aerodynamic estimation : an examination and validation for use in conceptual design /." Thesis, This resource online, 1993. http://scholar.lib.vt.edu/theses/available/etd-12052009-020129/.

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29

Robinson, Matthew J. "Simultaneous lift, moment and thrust measurement on a scramjet in hypervelocity flow /." [St. Lucia, Qld.], 2003. http://www.library.uq.edu.au/pdfserve.php?image=thesisabs/absthe17611.pdf.

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30

Lee, Jae-Moon. "Probabilistic inverse aerodynamic design optimization for natural laminar flow wings." Diss., Georgia Institute of Technology, 1999. http://hdl.handle.net/1853/11984.

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31

Bradshaw, Christopher John. "An experimental investigation of flapping wing aerodynamics in micro air vehicles." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2003. http://library.nps.navy.mil/uhtbin/hyperion-image/03Jun%5FBradshaw.pdf.

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Thesis (M.S. in Aeronautical Engineering)--Naval Postgraduate School, June 2003.<br>Thesis advisor(s): Kevin D. Jones, Max F. Platzer. Includes bibliographical references (p. 89). Also available online.

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32

Hubner, James Paul. "An investigation of quasiperiodic structures in the vortical flow over Delta wing configuration." Diss., Georgia Institute of Technology, 1995. http://hdl.handle.net/1853/12243.

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33

Elkoby, Ronen. "Acoustic excitation of wing wake flows." Thesis, Georgia Institute of Technology, 2000. http://hdl.handle.net/1853/12265.

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34

Hayne, Michael J. "Hypervelocity flow over rearward-facing steps /." [St. Lucia, Qld], 2004. http://www.library.uq.edu.au/pdfserve.php?image=thesisabs/absthe18242.pdf.

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35

Benoliel, Alexander M. "Aerodynamic pitch-up of cranked arrow wings : estimation, trim, and configuration design /." Thesis, This resource online, 1994. http://scholar.lib.vt.edu/theses/available/etd-11102009-020300/.

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36

Kuchan, Abigail. "The integration of active flow control devices into composite wing flaps." Thesis, Georgia Institute of Technology, 2012. http://hdl.handle.net/1853/44758.

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Delaying stall is always an attractive option in the aerospace industry. The major benefit of delaying stall is increased lift during takeoff and landings as well as during high angle of attack situations. Devices, such as fluidic oscillators, can be integrated into wing flaps to help delay the occurrence of stall by adding energized air to the airflow on the upper surface of the wing flap. The energized air from the oscillator allows the airflow to remain attached to the upper surface of the wing flap. The fluidic oscillator being integrated in this thesis is an active flow control device (A

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37

Huang, Ximing. "Structural optimization and its interaction with aerodynamic optimization for a high speed civil transport wing." Diss., Virginia Tech, 1994. http://hdl.handle.net/10919/40132.

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A variable-complexity design strategy with combined aerodynamic and structural optimization procedures is presented for the high speed civil transport design (HSCT). Variable-complexity analysis methods are used to reduce the computational expense. A finite element-model based structural optimization procedure with flexible loads is implemented to evaluate the wing bending material weight. Static aeroelastic effects, evaluated through the comparison of rigid and flexible wing models, are found to be small in the HSCT design. The results of structural optimization are compared with two quasi-em

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38

Zaki, Mina Adel. "Physics based modeling of axial compressor stall." Diss., Atlanta, Ga. : Georgia Institute of Technology, 2009. http://hdl.handle.net/1853/31683.

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Thesis (Ph.D)--Aerospace Engineering, Georgia Institute of Technology, 2010.<br>Committee Chair: Dr. Lakshmi N. Sankar; Committee Member: Dr. Alex Stein; Committee Member: Dr. J.V. R. Prasad; Committee Member: Dr. Richard Gaeta; Committee Member: Dr. Suresh Menon. Part of the SMARTech Electronic Thesis and Dissertation Collection.

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39

Bergen, Frederick D'Oench Jr. "Shape sensitivity analysis of flutter response of a laminated wing." Thesis, Virginia Polytechnic Institute and State University, 1988. http://hdl.handle.net/10919/50074.

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A method is presented for calculating the shape sensitivity of a wing aeroelastic response with respect to changes in geometric shape. Yates’ modified strip method is used in conjunction with Giles' equivalent plate analysis to predict the flutter speed, frequency, and reduced frequency of the wing. Three methods are used to calculate the sensitivity of the eigenvalue. The first method is purely a finite difference calculation of the eigenvalue derivative directly from the solution of the flutter problem corresponding to the two different values of the shape parameters. The second method uses

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40

Eveker, Kevin M. "Model Development for active control of stall phenomena in aircraft gas turbine engines." Diss., Georgia Institute of Technology, 1993. http://hdl.handle.net/1853/12363.

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41

Luo, Huageng. "Damage detection and health monitoring of structures using dynamic response and neural network techniques." Diss., Georgia Institute of Technology, 1996. http://hdl.handle.net/1853/12929.

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42

Miki, Kenji. "Simulation of magnetohydrodynamics turbulence with application to plasma-assisted supersonic combustion." Diss., Atlanta, Ga. : Georgia Institute of Technology, 2009. http://hdl.handle.net/1853/26605.

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Thesis (Ph.D)--Aerospace Engineering, Georgia Institute of Technology, 2009.<br>Committee Chair: Menon Suresh; Committee Co-Chair: Jagoda Jeff; Committee Member: Ruffin Stephen; Committee Member: Thorsten Stoesser; Committee Member: Walker Mitchell. Part of the SMARTech Electronic Thesis and Dissertation Collection.

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43

Patil, Mayuresh J. "Nonlinear aeroelastic analysis, flight dynamics, and control of a complete aircraft." Diss., Georgia Institute of Technology, 1999. http://hdl.handle.net/1853/12099.

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44

Zhang, Haochuan. "Nonlinear aeroelastic effects in damaged composite aerospace structures." Thesis, Georgia Institute of Technology, 1996. http://hdl.handle.net/1853/12150.

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45

Rowan, Scott A. "Viscous drag reduction in a scramjet combustor /." St. Lucia, Qld, 2003. http://www.library.uq.edu.au/pdfserve.php?image=thesisabs/absthe17438.pdf.

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46

Stewart, Benjamin S. "Predicted scramjet testing capabilities of the proposed RHYFL-X expansion tube /." [St. Lucia, Qld], 2004. http://www.library.uq.edu.au/pdfserve.php?image=thesisabs/absthe18241.pdf.

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47

Subramanian, Jagdeesh. "Aspect ratio effects on circular cylinder drag at low Reynolds numbers." Master's thesis, Mississippi State : Mississippi State University, 2005. http://sun.library.msstate.edu/ETD-db/ETD-browse/browse.

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48

Papay, Michael L. "A general inverse design procedure for aerodynamic bodies." Diss., Virginia Tech, 1994. http://hdl.handle.net/10919/38556.

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49

Carnegie, Cameron Lindsay Carleton University Dissertation Engineering Mechanical. "An Investigation into the aerodynamic effects of wing patches." Ottawa, 1992.

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50

Marx, William J. "Integrating design and manufacturing for the high speed civil transport." Diss., Georgia Institute of Technology, 1996. http://hdl.handle.net/1853/12410.

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