Three-Dimensional Integral Boundary Layer Formulation for General Configurations-Reference-Cited by-同舟云学术

Three-Dimensional Integral Boundary Layer Formulation for General Configurations

Published:2013-06-22 Issue: Volume: Page:
ISSN:
Container-title:21st AIAA Computational Fluid Dynamics Conference
language:
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Author:

Drela Mark¹

Affiliation:

1. Massachusetts Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-2437

Reference23 articles.

1. Viscous-inviscid analysis of transonic and low Reynolds number airfoils

2. XFOIL: An Analysis and Design System for Low Reynolds Number Airfoils

3. 3M.B. Bieterman, R.G. Melvin, F.T. Johnson, J.E. Bussoletti, D.P. Young, W.P. Huffman, C.L. Hilmes, and M. Drela. Boundary layer coupling in a general configuration full potential code. Technical Report BCSTECH-94-032, Boeing, Aug 1994.

4. Calculation of boundary-layer development using the turbulent energy equation: compressible flow on adiabatic walls

5. 5J.D. McLean and J.L. Randall. Computer program to calculate three-dimensional boundary layer flows over wings with wall mass transfer. NASA Contractor Report 3123, Boeing Company, Seattle, WA, 1979.

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