Flowfield of a lifting rotor in hover - A Navier-Stokes simulation
From MaRDI portal
Publication:4015297
DOI10.2514/3.11236zbMath0760.76065OpenAlexW2050377418MaRDI QIDQ4015297
W. J. McCroskey, Shigeru Obayashi, G. R. Srinivasan, James D. Baeder
Publication date: 11 January 1993
Published in: AIAA Journal (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.2514/3.11236
wakevortex structuregrid refinementimplicit, upwind, finite difference numerical methodsubsonic and transonic flow
Finite difference methods applied to problems in fluid mechanics (76M20) General theory of rotating fluids (76U05) Existence, uniqueness, and regularity theory for compressible fluids and gas dynamics (76N10)
Related Items
Multigrid convergence of inviscid fixed‐ and rotary‐wing flows ⋮ Rotorcraft simulations: a challenge for CFD ⋮ Numerical analysis of aerodynamic performance of rotors with leading edge slats ⋮ Aerodynamic shape optimization of hovering rotor blades using a nonlinear frequency domain approach ⋮ Development and preliminary assessment of the open-source CFD toolkit SU2 for rotorcraft flows ⋮ Improvements to a tightly coupled viscous-inviscid procedure for three-dimensional unsteady transonic flow. ⋮ Computationally fast harmonic balance methods for unsteady aerodynamic predictions of helicopter rotors ⋮ Upwind and central WENO schemes ⋮ Improving Godunov-type reconstructions for simulation of vortex-dominated flows ⋮ Convergence of steady and unsteady formulations for inviscid hovering rotor solutions ⋮ A multigrid Navier-Stokes CFD code for rotor computations ⋮ Short Communication: A Parallel Newton–Krylov Method for Navier–Stokes Rotorcraft Codes ⋮ Adaptive CFD analysis for rotorcraft aerodynamics ⋮ Numerical simulations of wake structure generated by rotating blades using a time marching, free vortex blob method
Uses Software
