3 edition of Numerical simulation of viscous supersonic flow over a generic fighter configuration found in the catalog.
Numerical simulation of viscous supersonic flow over a generic fighter configuration
D. S. Chaussee
by National Aeronautics and Space Administration, Ames Research Center, For Sale by the National Technical Information Service] in Moffett Field, Calif, [Springfield, Va
Written in English
|Statement||Denny S. Chaussee, Gordon Blom, John Wai.|
|Series||NASA technical memorandum -- 86823.|
|Contributions||Blom, Gordon., Wai, John., Ames Research Center.|
|The Physical Object|
Direct Numerical Simulation of Supersonic Turbulent Boundary Layer over a Compression Ramp M. Wu∗ and M. P. Martin† Princeton University, Princeton, New Jersey DOI: / A direct numerical simulation of shock wave andturbulent boundary layer interaction for a 24 deg compression rampconﬁgurationatMachandRe. Read "Supersonic, turbulent flow computation and drag optimization for axisymmetric afterbodies, Computers & Fluids" on DeepDyve, the largest online rental service for scholarly research with thousands of academic publications available at your fingertips.
Mar 02, · Effects of variable specific heat on energy transfer in a high-temperature supersonic channel flow. Journal of Turbulence, Vol. 19, Issue. 5, p. CrossRef; Direct Numerical Simulation of Acoustic Noise Generation from the Nozzle Wall of a Hypersonic H. P. Jr & Lumley, J. L. Viscous sublayer and adjacent wall region in turbulent Cited by: Andrea Farkas, Nastia Degiuli, Numerical simulation of viscous flow around a tanker model Ivana Martić of the ship resistance than potential flow methods . The main problem of viscous flow methods, beside turbulence modelling, is grid dependence, but this problem is Cited by: 3.
A numerical investigation of the performance of two candidate designs for injection into supersonic flow, including a comparison of two renormalized group theory (RNG) based k-epsilon turbulence models with a more conventional k-epsilon simplicityhsd.com by: 3. can perform quantitative simulation in CFD now. Robustness, reliability and computational eﬃciency of numerical algorithms have grown so much that CFD solvers can be used for blade shape optimisation. In the present paper the basic principles of modern approach of numerical simulation of 3D viscous turbomachinery ﬂows are described. 2.
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NUMERICAL SIMULATION OF VISCOUS SUPERSONIC FLOW OVER A GENERIC FIGHTER CONFIGURATION Denny S. Chaussee NASA Ames Research Center Moffett Field, CA USA Gordon Slom and John Wai Soeing Company Seattle, WA USA INTRODUCTION In the next generatlon of fighter alrcraft, the misslon requlrements.
A procedure is presented, as well as some results, to calculate the flow over a generic fighter configuration. A parabolized marching Navier-Stokes code is used to obtain the solution over a wing-canopy body. The flow conditions simulate supersonic cruise with a freestream Mach number of and angles of attack of 4 and 10 deg.
Get this from a library. Numerical simulation of viscous supersonic flow over a generic fighter configuration. [D S Chaussee; Gordon Blom; John Wai; Ames Research Center.]. High Reynolds number viscous transonic flow is described based on an interaction of the potential outer flow with the boundary layer and wake.
Numerical simulation of viscous transonic flows over an airfoil. Authors; Authors and affiliations Chow, R., and Mead, H., Theory of viscous transonic flow over airfoils at high Reynolds Cited by: 5.
Sep 16, · Various studies have been done on the computation of high-speed viscous flows over flat plates. Aliabadi et al.  presented a finite element-based computation of viscous compressible flows based upon the conservation and entropy variables simplicityhsd.comev  showed a numerical simulation of laminar viscous supersonic flow over a flat plate with a rectangular simplicityhsd.com by: 5.
law form. The numerical algorithm is applicable to steady supersonic viscous flow over bodies of arbitrary shape. In addition, the same code can be used to compute supersonic inviscid flow or three-dimensional boundary layers.
Computed results from two-dimensional and three-dimensional versions of the. numerical simulation of hypersonic viscous flow over a porous flat plate using finite volume method Article (PDF Available) · December with 83 Reads How we measure 'reads'. Efficient numerical method for simulation of supersonic viscous flow past a blunted body at a small angle of attack.
In Russian. Lin and S. Rubin, simplicityhsd.comional supersonic viscous flow over cone at incidence. AIAA Paper (). Dwyer, Grid adaption for problems in fluid dynamics.
AIAA J. 22(12), ().Cited by: Purpose – The paper seeks to perform a detailed numerical study of flow over a generic fan-wing airfoil and also attempts to modify the geometry for the improvement of the aerodynamic performance.
Numerical simulation of a supersonic compressible gas flow over different geometry bodies, namely, a flat plate, a hollow cylinder flare and a backward-facing step for different Reynolds numbers based on the numerical solution of the S-model of the Boltzmann equation is simplicityhsd.com by: 1.
Aug 14, · Computation of viscous flow for a Boeing aircraft in landing configuration. Stuart Rogers, Karlin Roth, Steven Nash, Numerical simulation of the interaction of MEMS actuators and boundary layers. Peter Carpenter, Three-dimensional supersonic flow over a flat-nosed body with a gasdynamic spike.
Algacyr Morgenstern, Jr. and. Computation of Supersonic Flow over Flying Configurations is a high-level aerospace reference book that will be useful for undergraduate and graduate students of engineering, applied mathematics and simplicityhsd.com author provides solutions for three-dimensional compressible Navier-Stokes layer subsonic and supersonic flows.
Simulation of transonic viscous flow over a fighter-like configuration including inlet. JOLEN FLORES, Experimental study of the vortex flow behavior on a generic fighter wing at subsonic and transonic speeds.
GARY ERICKSON and; Numerical simulation of supersonic flow over a three-dimensional cavity. DONALD RIZZETTA. Numerical simulation of supersonic viscous flow based on adaptive Cartesian grid TANG Zhigong, CHEN Hao, BI Lin, YUAN Xianxu TANG Zhigong, CHEN Hao, BI Lin, YUAN Xianxu. Numerical simulation of supersonic viscous flow based on adaptive Cartesian grid[J].
ACTA AERONAUTICAET ASTRONAUTICA SINICA,39(5): EFFICIENT NUMERICAL METHOD FOR SIMULATION OF SUPERSONIC VISCOUS FLOW PAST A BLUNTED BODY AT A SMALL ANGLE OF ATTACK G. TmsKn, S. UTYUZHNIKOV~ and N. YAMALEEV Department of Computational Mathematics, Moscow Institute of Physics & Technology, Dolgoprudny, MoscowRussia.
The stepback and partial grid techniques were used in the numerical simulation of laminar viscous reacting flows past cones at incidence. The stepback technique is a method for computing exactly flows which are truly conical, and can be an effective approximate method for nearly conical flows such as viscous flow past simplicityhsd.com: Shaun Shariff.
Over the last decade, considering the influence of the viscous free water surface, the numerical simulation of the flow around the hull is one of the focuses in ship research.
Currently, the precision of numerical simulation results need to be enhanced. In this paper, Computational Fluid Dynamics (CFD) method is used, for a real high-speed ship model, to simulate the flow around the hull and Cited by: 1.
Characteristics of flow. While the definition of hypersonic flow can be quite vague and is generally debatable (especially due to the absence of discontinuity between supersonic and hypersonic flows), a hypersonic flow may be characterized by certain physical phenomena that can no longer be analytically discounted as in supersonic flow.
Y.M. Rizk, L.B. Schiff, K. Gee, and R.M. Cummings, "Numerical Simulation of the Viscous Flow Around the F at High Angles of Attack," AIAA 8th Applied Aerodynamics Conference, Portland OR, AIAA PaperAug This paper investigates both experimentally and numerically the flow of a viscous fluid around T-profiles, i.e.
T-shaped bodies, having different geometries. Of main interest it was the vortex shedding behind the T-profiles with an eye towards its application to flow measurement in open channels. Another purpose of the study was to assess to what extent different numerical models can be used Author: Mihai Schiaua, Andrei Dragomirescu, Carmen Anca Safta.
Apr 01, · This paper focuses on the numerical simulations of flow around a realistic generic car model called the DrivAer body. This new open-source model is based on the geometries of two medium sized cars, the Audi A4 and the BMW 3 series, and possesses more representative car features as the well-known generic Ahmed simplicityhsd.com by: Numerical simulation of viscous supersonic flow over a generic fighter configuration [microform] / Denny Calculation of steady flow through a channel with a sudden expansion using the SIMPLEC method / Faris S.
Calculation of properties using corresponding-state methods / .Jan 28, · Numerical Computation of Compressible and Viscous Flow (AIAA Education Series) [Robert W.
MacCormack] on simplicityhsd.com *FREE* shipping on qualifying offers. Numerical Computation of Compressible and Viscous is written for those who want to calculate compressible and viscous flow past aerodynamic bodies.
As taught by Robert W. MacCormack at Stanford University/5(2).