Calculation of external-internal flow fields for mixed-compression inlets

DOI10.1016/0045-7825(87)90031-4zbMath0607.76062OpenAlexW1995167149MaRDI QIDQ1085732

B. George

Publication date: 1987

Published in: Computer Methods in Applied Mechanics and Engineering (Search for Journal in Brave)

Full work available at URL: http://hdl.handle.net/2060/19870015001

zbMATH Keywords

conservation formcombined implicit-explicit methodcowl lipmixed external-internal compressionsshock-wave intersectionssubsonic spillagesupersonic inlet flowsthree-dimensional unsteady, compressible Navier-Stokes equations

Mathematics Subject Classification ID

Navier-Stokes equations (35Q30) Existence, uniqueness, and regularity theory for compressible fluids and gas dynamics (76N10) Supersonic flows (76J20) Basic methods in fluid mechanics (76M99)

Cites Work

• Boundary treatments for implicit solutions to Euler and Navier-Stokes equations
• Three-dimensional flow simulations for supersonic mixed-compression inlets at incidence
• Two-Dimensional Inlet Simulation Using a Diagonal Implicit Algorithm
• Calculation of Transonic Flow around Axisymmetric Inlets
• Transonic Potential Flow around Axisymmetric Inlets and Bodies at Angle of Attack
• Cartesian Mesh Solution for Axisymmetric Transonic Potential Flow Around Inlets
• Accelerated Iterative Calculation of Transonic Nacelle Flowfields
• Implicit Finite-Difference Simulation of Flow about Arbitrary Two-Dimensional Geometries

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