Flight vehicle aerodynamics calculated by a Galerkin finite element/finite difference method-Reference-Cited by-同舟云学术

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Flight vehicle aerodynamics calculated by a Galerkin finite element/finite difference method

Published:1992-01 Issue:1-4 Volume:3 Page:413-421
ISSN:0956-0521
Container-title:Computing Systems in Engineering
language:en
Short-container-title:Computing Systems in Engineering

Author:

Holt M.,Meade A.J.

Publisher

Elsevier BV

Subject

General Engineering

Reference34 articles.

1. W. S. Helliwell and S. C. Lubard, “An implicit method for three-dimensional viscous flow with application to cones at angle of attack,” Aerospace Corp. Report TR-0074(4450-64)-1.

2. Supersonic viscous flow over cones at incidence;McRae,1978

3. Computation of asymmetric supersonic flows around cones at large incidence;Degani,1987

4. On supersonic flow around a slightly yawed cone, Part I;Stone;Journal of Mathematics and Physics,1948

5. On supersonic flow around a slightly yawed cone, Part II;Stone;Journal of Mathematics and Physics,1952

Cited by 1 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. A Multifunctional Interface Method for Coupling Finite Element and Finite Difference Methods: Two-Dimensional Scalar-Field Problems;43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2002-04-22

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