Numerical simulation of unsteady, viscous, high-angle-of-attack flows using a partially flux-split algorithm-Reference-Cited by-同舟云学术

Numerical simulation of unsteady, viscous, high-angle-of-attack flows using a partially flux-split algorithm

Published:1986-08-17 Issue: Volume: Page:
ISSN:
Container-title:Astrodynamics Conference
language:
Short-container-title:

Author:

YING S.¹,BAGANOFF D.¹,STEGER J.²,SCHIFF L.²

Affiliation:

1. Stanford University, CA

2. NASA, Ames Research Center, Moffett Field, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1986-2179

Reference25 articles.

1. Flux vector splitting of the inviscid gasdynamic equations with application to finite-difference methods

2. Developments in the Simulation of Compressible Inviscid and Viscous Flow on Supercomputers

3. Buning, P. G. "Computation of InviscidTransonicFlowUsingFluxVector Splitting in Generalized Coordinates,*PhD. Thesis,Stanford University, 1983. Baldwin, B. S. and Lomax, H. "Thin Layer Approximation and Algebraic Modelfor Separated Turbulent Flows," AIAA Paper 78-257, 1978.

4. Implicit Finite-Difference Simulation of Flow about Arbitrary Two-Dimensional Geometries

5. to 1.5," AEDC-TR-76-112,1976. *. Hsieh, T. "Hemisphere-Cylinder in Low Su

Cited by 62 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Flow around a hemisphere-cylinder at high angle of attack and low Reynolds number. Part I: Experimental and numerical investigation;Aerospace Science and Technology;2015-07

2. Numerical and experimental investigation of unsteady three-dimensional separation on axisymmetric bodies;International Journal of Heat and Fluid Flow;2013-12

3. An Investigation of a Slender Forebody Maneuvering at Incidence in High Reynolds Number Flow;44th AIAA Aerospace Sciences Meeting and Exhibit;2006-01-09

4. Projectile Performance, Stability, and Free-Flight Motion Prediction Using Computational Fluid Dynamics;Journal of Spacecraft and Rockets;2004-03

5. Numerical Investigation of Supersonic Jet Interaction for Finned Bodies;Journal of Spacecraft and Rockets;2002-05