HISSS - A higher-order subsonic/supersonic singularity method for calculating linearized potential flow-Reference-Cited by-同舟云学术

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HISSS - A higher-order subsonic/supersonic singularity method for calculating linearized potential flow

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

Author:

FORNASIER L.¹

Affiliation:

1. Messerschmitt-Boelkow-Blohm GmbH, Ottobrunn, West Germany

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1984-1646

Cited by 16 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. Implementation of MachLine: A Subsonic/Supersonic, Unstructured Panel Code;AIAA SCITECH 2023 Forum;2023-01-19

2. Development of a Subsonic-Supersonic, Unstructured Panel Method;AIAA SCITECH 2022 Forum;2022-01-03

3. Large Aspect-Ratio Wing Flow;Separated and Vortical Flow in Aircraft Wing Aerodynamics;2020-10-05

4. A Higher-Order Method Implemented in an Unstructured Panel Code to Model Linearized Supersonic Flows;AIAA Scitech 2020 Forum;2020-01-05

5. Illustrating Examples;Three-Dimensional Attached Viscous Flow;2014

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