Computation of turbulent flow in a mixed compression intake
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[1] D. Herrmann,et al. Experimental Analyses of Inlet Characteristics of an Airbreathing Missile with Boundary-Layer Bleed , 2015 .
[2] V. M. Krushnarao Kotteda,et al. Stabilized finite‐element computation of compressible flow with linear and quadratic interpolation functions , 2014 .
[3] Boniface Nkonga,et al. A fully coupled RANS Spalart–Allmaras SUPG formulation for turbulent compressible flows on stretched-unstructured grids , 2012 .
[4] V. M. Krushnarao Kotteda,et al. Viscous flow in a mixed compression intake , 2011 .
[5] In-Seuck Jeung,et al. Flow Characteristics of Small-Sized Supersonic Inlets , 2011 .
[6] Sanjay Mittal,et al. Buzz Instability in a Mixed-Compression Air Intake , 2009 .
[7] Sébastien Deck,et al. Delayed Detached-Eddy Simulation and Analysis of Supersonic Inlet Buzz , 2008 .
[8] Sébastien Deck,et al. Experimental Study of Supersonic Inlet Buzz , 2006 .
[9] Sanjay Mittal,et al. Euler flow in a supersonic mixed‐compression inlet , 2006 .
[10] S. Mittal,et al. Flow past a rotating cylinder , 2003, Journal of Fluid Mechanics.
[11] Tayfun E. Tezduyar,et al. Stabilization Parameters and Smagorinsky Turbulence Model , 2003 .
[12] B. E. Launder,et al. Closure Strategies for Turbulent and Transitional Flows , 2002 .
[13] S. Deck,et al. Development and application of Spalart–Allmaras one equation turbulence model to three-dimensional supersonic complex configurations , 2002 .
[14] Stuart E. Rogers,et al. Advances in overset CFD processes applied to subsonic high-lift aircraft , 2000 .
[15] C. Gacherieu,et al. Assessment of Algebraic and One-Equation Turbulence Models for the Transonic Turbulent Flow around a Full Aircraft Configuration , 1998 .
[16] Sanjay Mittal,et al. Finite element computation of unsteady viscous compressible flows , 1998 .
[17] Sanjay Mittal,et al. Finite element computation of unsteady viscous transonic flows past stationary airfoils , 1998 .
[18] Pong-Jeu Lu,et al. Numerical Investigation of Inlet Buzz Flow , 1998 .
[19] P. Spalart. A One-Equation Turbulence Model for Aerodynamic Flows , 1992 .
[20] S. Liang,et al. Numerical investigation of supersonic mixed-compression inlet using an implicit upwind scheme , 1992 .
[21] Tayfun E. Tezduyar,et al. Finite element computation of compressible flows with the SUPG formulation , 1991 .
[22] T. Hughes,et al. Streamline upwind/Petrov-Galerkin formulations for convection dominated flows with particular emphasis on the incompressible Navier-Stokes equations , 1990 .
[23] Kazuomi Yamamoto,et al. A numerical investigation of supersonic inlet using implicit TVD scheme , 1990 .
[24] Y. Saad,et al. GMRES: a generalized minimal residual algorithm for solving nonsymmetric linear systems , 1986 .
[25] T. Hughes,et al. A new finite element formulation for computational fluid dynamics: II. Beyond SUPG , 1986 .
[26] Mizukami Akira,et al. An implementation of the streamline-upwind/petrovgalerkin method for linear triangular elements☆ , 1985 .
[27] R. Newsome,et al. Numerical Simulation of Near-Critical and Unsteady, Subcritical Inlet Flow , 1984 .
[28] Doyle Knight,et al. Calculation of a simulated 3-D high speed inlet using the Navier-Stokes equations , 1983 .
[29] Thomas J. R. Hughes,et al. Finite element formulations for convection dominated flows with particular emphasis on the compressible Euler equations , 1983 .
[30] D. Knight. Improved Calculation of High Speed Inlet Flows. Part II: Results , 1981 .
[31] T. Hughes,et al. MULTI-DIMENSIONAL UPWIND SCHEME WITH NO CROSSWIND DIFFUSION. , 1979 .
[32] N. D. Wong,et al. Experimental investigation of a large scale, two-dimensional, mixed-compression inlet system - Performance at design conditions, M=3.0 , 1970 .
[33] S. Fisher,et al. On the SubCritical Stability of Variable Ramp Intakes at Mach Numbers Around 2 By , 1970 .
[34] R. L. Trimpi,et al. A Theory for Stability and Buzz Pulsation Amplitude in Ram Jets and an Experimental Investigation Including Scale Effects , 1956 .
[35] Charles Lee Dailey,et al. Supersonic Diffuser Instability , 1955 .
[36] Antonio Ferri,et al. The Origin of Aerodynamic Instability of Supersonic Inlets at Subcritical Conditions , 1951 .