Newton method on axisymmetric transonic flow and linearized 3D flow prediction-Reference-Cited by-同舟云学术

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Newton method on axisymmetric transonic flow and linearized 3D flow prediction

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

Author:

Ahn Jon¹,Drela Mark²

Affiliation:

1. Korea Inst. of Aeronautical Technology, Taejon, Republic of Korea

2. MIT, Cambridge, MA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-928

Reference16 articles.

1. The Theory of Thin Wings in Subsonic Flow

2. 4Drela, M. "Viscousand InviscidInverseSchemes UsingNewton'sMethod" AGARDReport AGARDR-780, Special Course on Inverse Methods for Airfoil Designfor Aeronautical and Turbomachinery Applications, 1990.

3. 5Drela, M. Two-Dimensional Transonic Aerodynamic Design and Analysis Using the Euler Equations, Ph.D. thesis,MIT,1985.

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