Computation of transonic viscous airfoil, inlet, and wing flowfields-Reference-Cited by-同舟云学术

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Computation of transonic viscous airfoil, inlet, and wing flowfields

Published:1984-06-25 Issue: Volume: Page:
ISSN:
Container-title:17th Fluid Dynamics, Plasma Dynamics, and Lasers Conference
language:
Short-container-title:

Author:

AGARWAL R.¹,DEESE J.¹

Affiliation:

1. McDonnell Douglas Research Laboratories, St. Louis, MO

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1984-1551

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. Evaluation of a multigrid-based Navier-Stokes solver for aerothermodynamic computations;Journal of Spacecraft and Rockets;1995-03

2. A massively parallel three-dimensional Euler/Navier-Stokes method;9th Computational Fluid Dynamics Conference;1989-06-13

3. Development of an efficient multigrid code for 3-D Navier-Stokes equations;20th Fluid Dynamics, Plasma Dynamics and Lasers Conference;1989-06-12

4. A coupled Euler/Navier-Stokes algorithm for 2-D unsteady transonic flows;27th Aerospace Sciences Meeting;1989-01-09

5. Accurate numerical solutions for transonic viscous flow over finite wings;Journal of Aircraft;1987-06

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