Relevant bibliographies by topics / Detonation waves. Aerodynamics, Hypersonic. Fluid dynamics

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Academic literature on the topic 'Detonation waves. Aerodynamics, Hypersonic. Fluid dynamics'

Author: Grafiati
Published: 4 June 2021
Last updated: 16 February 2022

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Dissertations / Theses on the topic "Detonation waves. Aerodynamics, Hypersonic. Fluid dynamics"

1

Fort, James A. "A numerical study of attached oblique detonation /." Thesis, Connect to this title online; UW restricted, 1993. http://hdl.handle.net/1773/7087.

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2

(11022453), Akshay Deshpande. "Unsteady Dynamics of Shock-Wave Boundary-Layer Interactions." Thesis, 2021.

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<div>Shock-wave/turbulent boundary-layer interactions (SWTBLIs) are characterized by low-frequency unsteadiness, amplified aerothermal loads, and a complex three-dimensional flowfield. Presence of a broad range of length and time-scales associated with compressible turbulence generates additional gasdynamic features that interact with different parts of the flowfield via feedback mechanisms. Determining the physics of such flows is of practical importance as they occur frequently in different components of a supersonic/hypersonic aircraft such as inlets operating in both on- and off-design con
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(10586768), Bhavini Singh. "Spark induced flow in quiescent air." Thesis, 2021.

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<p>Nanosecond spark plasma actuators provide an opportunity to reduce pollutants by promoting efficient combustion in engines or provide targeted, tunable, flow control over vehicles, due to their ability to influence flow and combustion through multiple mechanisms. The plasma actuators can be physically unobtrusive, can be turned on and off and their low duty cycle, large bandwidth, and light weight make them more appealing than other control approaches. One method by which these plasma actuators interact with the environment is by inducing a complex local flow field and in order, to design s
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Books on the topic "Detonation waves. Aerodynamics, Hypersonic. Fluid dynamics"

1

Arthur, Rizzi, and Hirschel Ernst-Heinrich, eds. Numerical solutions of the Euler equations for steady flow problems. Vieweg, 1991.

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Eberle, Albrecht. Numerical solutions of the Euler equations for steady flow problems. Vieweg, 1992.

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3

Holland, Scott D. Mach 10 experimental database of a three-dimensional scramjet inlet flow field. National Aeronautics and Space Administration, Langley Research Center, 1995.

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Krishnan, Radhakrishnan, ed. Computational study of flow establishment in hypersonic pulse facilities. National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion, 1995.

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Center, Langley Research, ed. Mach 10 experimental database of a three-dimensional scramjet inlet flow field. National Aeronautics and Space Administration, Langley Research Center, 1995.

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