Multiple‐Zone Potential Solution around Wing‐Body Configurations-Reference-Cited by-同舟云学术

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Multiple‐Zone Potential Solution around Wing‐Body Configurations

Published:1993-10 Issue:4 Volume:6 Page:329-346
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:Journal of Aerospace Engineering

Author:

Alishahi M. M.,Darbandi M.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%290893-1321%281993%296%3A4%28329%29

Reference15 articles.

1. Numerical Procedure for the Computation of Irrotational Conical Flows

2. Karimian S. M. H. (1990). “Numerical solution of full potential transonic equation about arbitrary airfoils ” MS thesis Sharif Univ. of Tech. Tehran Iran.

3. Supersonic noncircular missile computations

4. Rai M. M. (1984). “A conservative treatment of zonal boundaries for Euler equations.” AIAA Paper 84‐0164 American Inst. of Aeronautics and Astronomics New York N.Y.

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1. Developing Consistent Inlet Boundary Conditions to Study the Entrance Zone in Microchannels;Journal of Thermophysics and Heat Transfer;2007-07

2. Multiblock hybrid grid finite volume method to solve flow in irregular geometries;Computer Methods in Applied Mechanics and Engineering;2006-12

3. Development of a Consistent Slip-Boundary Condition at the Inlet of Microchannels;44th AIAA Aerospace Sciences Meeting and Exhibit;2006-01-09

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