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21	Double reduction of partial differential equations with applications to laminar jets and wakes Kokela, Lady Nomvula January 2016 (has links) A dissertation submitted to the Faculty of Science, School of Computational and Applied Mathematics, University of the Witwatersrand, Johannesburg, in fulfilment of requirements for the degree of Master of Science. Johannesburg, 2015. / Invariant solutions for two-dimensional free and wall jets are derived by consid- ering the Lie point symmetry associated with the appropriate conserved vectors of Prandtl's boundary layer equations for the jets. For the two-dimensional jets we also consider the comparison, advantages and disadvantages between the standard method that uses a linear combination of all the Lie point symme- tries of Prandtl's boundary layer equations to generate the invariant solution with the new method explored in this paper which uses the Lie point sym- metry associated with a conserved vector to generate the invariant solution. Invariant solutions for two-dimensional classical and self-propelled wakes are also derived by considering the Lie point symmetry associated with the appro- priate conserved vectors of Prandtl's boundary layer equations for the wakes. We also consider and discuss the standard method that uses a linear combi- nation of all the Lie point symmetry of Prandtl's boundary layer equations to generate the invariant solutions for the classical and self-propelled wakes. Differential equations, Partial. Wakes (Aerodynamics) Jets.
22	Computation of helicopter rotor wake geometry and its influence on rotor harmonic airloads Scully, M. (Michael) January 1975 (has links) Thesis. 1975. Ph.D.--Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. / Vita. / Includes bibliographical references. / by Michael P. Scully. / Ph.D. Aeronautics and Astronautics Rotors (Helicopters) Aerodynamics Wakes (Aerodynamics)
23	Circulation control for download wake reduction on a scaled V-22 model Riba, Chad Alan. January 2003 (has links) Thesis (M.S.)--West Virginia University, 2003. / Title from document title page. Document formatted into pages; contains x, 87 p. : ill. (some col.). Includes abstract. Includes bibliographical references (p. 72-73).
24	Wake induced transition in low pressure turbines Coull, John David January 2010 (has links) No description available. 620
25	Helicopter rotor dynamic inflow modeling for maneuvering flight Krothapalli, Krishnamohan Rao 08 1900 (has links) No description available. Rotors Dynamics Helicopter flight simulators Wakes (Aerodynamics)
26	Acoustic excitation of wing wake flows Elkoby, Ronen 12 1900 (has links) No description available. Wakes (Aerodynamics) Measurement Noise Airplanes Wings
27	An improved method of calculating the tip vortex geometry for hovering rotors Samant, Satish Shripad 12 1900 (has links) No description available. Vortex-motion Wakes (Aerodynamics) Rotors (Helicopters)
28	An integrated Navier Stokes-full portential-free wake method for rotor flows Berkman, Mert Enis 05 1900 (has links) No description available. Wakes (Aerodynamics) Rotors Dynamics Navier-Stokes equations
29	A theory of the supersonic turbulent axisymmetric near wake behind bluff-base bodies Mehta, Gopal Krishna 05 1900 (has links) No description available. Base flow (Aerodynamics) Drag (Aerodynamics) Wakes (Aerodynamics)
30	Computation of wake-passing effects on turbine blade boundary layers / Kim, Kyoungjin, January 1998 (has links) Thesis (Ph. D.)--University of Texas at Austin, 1998. / Vita. Includes bibliographical references (leaves 152-157). Available also in a digital version from Dissertation Abstracts.

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