Know your flow - The key to better prediction and successful innovation-Reference-Cited by-同舟云学术

Know your flow - The key to better prediction and successful innovation

Published:1998-01-12 Issue: Volume: Page:
ISSN:
Container-title:36th AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Haines A.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-221

Reference28 articles.

1. Shaw,JA,Peace,AJ,May,NE and Pocock,MF ."Verification of the CFD System SAUNA for Complex Aircraft Configurations ",AIAA-94-0393,January 1994

2. Peace,AJ,May NE, Pocock MF and Shaw JA "Inviscid and ViscousFlow Modelling of Complex Aircraft Configurations using the CFD Simulation SystemSAUNA",ICAS-94-2.6.3,September 1994

3. Peace,AJ, Chappell JA and Shaw JA "TurbulentFlow Calculations forComplexAircraft Geometries using Prismatic Grid Regions in the SAUNACFDcode",ICAS-96-1.4.2.,1996

4. Szmelter,J "Viscous Coupling Techniques usingUnstructured and Multiblock Meshes"ICAS96-1.7.4, 1996

Cited by 7 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. Study of Plasma-Based Vortex Generator in Supersonic Turbulent Boundary Layer;Aerospace;2023-04-10

2. The potential of hybrid micro-vortex generators to control flow separation of NACA 4415 airfoil in subsonic flow;AIP Conference Proceedings;2018

3. Review of research on low-profile vortex generators to control boundary-layer separation;Progress in Aerospace Sciences;2002-05

4. Prediction of scale effects at transonic speeds: current practice and a gaze into the future;The Aeronautical Journal;2000-09

5. Recent experience with different methods of drag prediction;Progress in Aerospace Sciences;1999-11