Implicit Finite-Difference Computations of Unsteady Transonic Flows about Airfoils

DOI10.2514/3.60838zbMath0394.76008OpenAlexW1628157360MaRDI QIDQ4177177

Peter M. Goorjian, William F. Jun. Ballhaus

Publication date: 1977

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.60838

zbMATH Keywords

Finite Difference MethodDisturbance EquationNonlinear ResultsSolution AlgorithmTijdeman's Experimental Observations of Shock Wave Motions

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Transonic flows (76H05) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10) Numerical solution of discretized equations for boundary value problems involving PDEs (65N22)

Related Items (11)

AN UNFACTORED IMPLICIT MOVING MESH METHOD FOR THE TWO-DIMENSIONAL UNSTEADY N-S EQUATIONS ⋮ A Mach-sensitive implicit-explicit scheme adapted to compressible multi-scale flows ⋮ Stable and Entropy Satisfying Approximations for Transonic Flow Calculations ⋮ Finite element methodology for modeling aircraft aerodynamics: development, simulation, and validation ⋮ Aeroelastic time response analysis of thin airfoils by transonic code LTRAN 2 ⋮ Far field boundary conditions for compressible flows ⋮ Time domain numerical calculations of unsteady vortical flows about a flat plate airfoil ⋮ The Spectrum and the Stability of the Chebyshev Collocation Operator for Transonic Flow ⋮ The mathematical approach to the sonic barrier ⋮ A least squares finite element scheme for transonic flow around harmonically oscillating airfoils ⋮ Flow in the neighbourhood of the trailing edge of a plate in a transonic flow of viscous gas

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