Effects of vibrational nonequilibrium on the inviscid design of an axisymmetric nozzle for hypersonic flow [PDF]
An axisymmetric, hypersonic nozzle for arc-heated air is described. The method of characteristics is used to compute an inviscid nozzle contour in which vibrational nonequilibrium is approximated by the sudden-freeze technique.
Anders, J. B., Jr.
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The wall shear stress produced by the normal impingement of a jet on a flat surface [PDF]
, 2000 A method for the theoretical determination of the wall shear stress under impinging jets of various congurations is presented. Axisymmetric and two-dimensional incompressible jets of a wide range of Reynolds numbers and jet heights are considered ...
Flagan, Richard C. +2 more
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Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability [PDF]
A static investigation of the internal performance of two short take-off and landing (STOL) nozzle concepts with pitch thrust-vectoring capability has been conducted.
Burley, J. R., II, Mason, M. L.
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Dynamics and Control of Drop Formation, Detachment, and Post-Detachment Oscillations-Computational Simulation, Using a Conservative Phase Field Model in Lattice Boltzmann Method [PDF]
Journal of Applied and Computational MechanicsThis research numerically studies the dynamics and control of formation, detachment, and post-oscillations of a two-dimensional drop, using the Lattice Boltzmann Method (LBM) with a Conservative Phase Field (CPF) model. The problem is formulated for drop
Yaser Jafari +3 more
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Turbulent jet characteristics for axisymmetric and serrated nozzles [PDF]
Computers & Fluids, 2015 zbMATH Open Web Interface contents unavailable due to conflicting licenses.
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Numerical study of acoustic oscillations and combustion instabilities in solid propellant rocket [PDF]
, 1997 A numerical analysis of unsteady motions in solid rocket motors has been conducted. A fully coupled implicit scheme based on a dual time-stepping integration algorithm has been adopted to solve the governing equations and associated boundary conditions.
Culick, F. E. C., Roh, T. S.
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Numerical Study of Subsonic Hot and Near-Sonic Submerged Jets Based on a Two-Fluid Model [PDF]
Journal of Applied and Computational MechanicsThis paper discusses the hot subsonic and near-sonic axisymmetric submerged stationary jets flowing from a nozzle with a radius of 25.4 mm. The Mach number at the nozzle exit is 0.376 for a subsonic jet, and for a near-sonic jet, it is 0.985.
Zafar Malikov +2 more
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FluidsThe current study explores the flowfield and noise characteristics of an ideally expanded supersonic (Mach 1.44) rectangular jet impinging on a flat surface.
Yogesh Mehta +2 more
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Experimental and Theoretical Investigations of Edge Tones in High Speed Jets
Journal of Fluid Science and Technology, 2013 Experimental and theoretical investigations of the high speed jets impinge on a wedge-shaped edge have been conducted. Sonic circular and square jets of the same hydraulic diameter are examined in the present study.
Mohammed K. IBRAHIM
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A method for calculating a real-gas two-dimensional nozzle contour including the effects of gamma [PDF]
A method for calculating two-dimensional inviscid nozzle contours for a real gas or an ideal gas by the method of characteristics is described. The method consists of a modification of an existing nozzle computer program. The ideal-gas nozzle contour can
Boney, L. R., Johnson, C. B.
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