A new boundary-layer inviscid iteration technique for separated flow-Reference-Cited by-同舟云学术

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A new boundary-layer inviscid iteration technique for separated flow

Published:1979-07-23 Issue: Volume: Page:
ISSN:
Container-title:4th Computational Fluid Dynamics Conference
language:
Short-container-title:

Author:

CARTER J.¹

Affiliation:

1. NASA, Langley Research Center, Hampton, Va.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1979-1450

Reference24 articles.

1. Supercritical Wing Sections II

2. Carter, James E.; and Wornom, Stephen F.: Solutions for Incompressible Separated Boundary Layers Including Viscous-Inviscid Interaction. Aerodynamic Analyses Requiring Advanced Computers, Part I. NASA SF-347, pp.125-150.

3. Davis, R. T.; and Werle, M. J.: Numerical Methods for Interacting Boundary Layers. Univ. of Cincinnati Rept. No. AFL 76-8-23, Aug. 1976

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