Progress in Flight Physics – Volume 3
Versailles, France, July 6-10, 2009Ph. Reijasse, D.D. Knight, M.S. Ivanov and I.I. Lipatov (Eds.)
ISBN: 978-2-7598-0674-4
Chapter One. Aerodynamics
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Preliminary results of flow fluctuation measurements in the cryogenic transonic wind tunnel p. 3
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Temperature sensitive paint application for investigation of boundary layer transition in short-duration wind tunnels p. 15
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Simulation of afterbody transonic flows using partially-averaged navier stokes model for turbulence p. 25
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Flow structure and turbulence in near fields of circular and noncircular jets p. 41
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Aircraft dynamic lateral stability analytic formulation for dutch roll mode stability prediction p. 53
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A joint numerical and experimental study of the jet of an aircraft engine installation with advanced techniques p. 63
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Propagation of disturbance in boundary layer on planar delta wing in the strong interaction regime p. 79
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Explicit algebraic reynolds stress models for anisotropic wall-bounded flows p. 89
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Chapter Two. Shock Interaction
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Low and high enthalpy shock wave / boundary layer interactions around cylinder-flare models p. 107
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Numerical prediction of three-dimensional shock-induced turbulent flow separation surrounding bodies of revolution adjacent to a flat surface p. 119
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Effect on a shock wave boundary layer interaction of air jet vortex generators p. 141
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Numerical study of three-dimensional modulations in a shock-induced separation p. 157
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Numerical simulation of shock-induced separated flows in overexpanded rocket nozzles p. 169
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Chapter Three. High Enthalpy Flows
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Development of a compact electron beam fluorescence instrument for high enthalpy flow characterization p. 193
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Active control of hypersonic shock layer disturbances p. 205
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Evaluation of nonequilibrium boundary conditions for hypersonic rarefied gas flows p. 217
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Experimental study and numerical modeling of vibrational oxygen temperature profiles behind a strong shock wave front p. 231
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Hypersonic laminar/turbulent transition: computations and experiments p. 243
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Dependence and sensitivity on the aerothermochemical model of atmospheric reentry trajectories p. 253
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Chemical nonequilibrium effects in the wake of an obstacle in hypersonic boundary-layer flows p. 267
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Aerothermodynamics of expert ballistic vehicle at hypersonic speeds p. 277
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Experiments on hypersonic boundary layer transition on blunt cones with acoustic-absorption coating p. 295
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Chapter Four. Heat Transfer
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Laminar-turbulent flow around a wedge placed on sharp and blunted plates p. 307
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The tangential gas injection as the means of heat protection of a blunt body streamlined by dusted gas p. 321
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Experimental studies of Pre-X vehicle heat transfer in PGU-7 test facility p. 335
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Simulation of oxygen atom heterogeneous recombination on Al2O3 from ab initio approach p. 351
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The methology for determination of catalytic properties of SiC samples for specified Pre-X and MSRO conditions p. 365
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Navier-Stokes analysis of scale effects on ablation in carbon-carbon rocket nozzles p. 381
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Peculiarities of flow and heat transfer in the base region of generic model of martian descent vehicle p. 395
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Chapter Five. Aeroacoustics
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Acoustic environment resulting in interaction of launch vehicle main engines jets with a launch pad having closed long ducts like a tunnel p. 405
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Reynolds number effect in a problem of sound generation by round and truncated cylinder streamlined by turbulent flow p. 421
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Development of a free round jet at different conditions at the nozzle exit under an acoustic action p. 429
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Chapter Six. Flow Control
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Convective instabilities in a backward-facing step flow: global forced perturbations p. 451
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Adjoint-based control of afterbody flow unsteadiness in the compressible regime p. 461
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Model reduction and control of a separating boundary-layer flow p. 471
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Asymptotical models of boundary layer flow control p. 483
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Global stability analysis - a key enabler in reduced order models and flow control p. 491
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Reduced order models for closed loop control: comparison between POD, BPOD, and global modes p. 503
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Investigation of cross flow forces influence on incompressible laminar flow p. 513
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Numerical modeling of separated flows in three-dimensional diffusers and application of synthetic jets for separation control p. 521
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Experimental and numerical studies of nonequilibrium effects in framework of magnetohydrodynamic parachute concept p. 529
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Study of the incipient spot breakdown controlled by riblets p. 545
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Flow control in a supersonic inlet model by electrical discharge p. 557
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