Boundary-Layer Control by Electric Fields
Author:
Affiliation:
1. Grupo de Fi´sica-Matema´tica, Complexo II, Universidade de Lisboa, Av. Gama Pinto 2, 1699 Lisboa Codex, Portugal
2. Laborato´rio de Mecatro´nica, DEEC, Instituto Superior Te´cnico, Av. Rovisco Pais, 1096 Lisboa Codex, Portugal
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/fluidsengineering/article-pdf/120/3/626/5901030/626_1.pdf
Reference11 articles.
1. Blottner F. G. , 1970, “Finite Difference Methods of Solution of the Boundary-Layer Equations,” AIAA Journal, Vol. 8, pp. 193–205.
2. Davis R. T. , 1970, “Numerical Solution of the Hypersonic Viscous Shock-Layer Equations,” AIAA Journal, Vol. 8, pp. 843–851.
3. Gailitis A. K. , and LielausisO. A., 1961, “On the Possibility of Drag Reduction of a Flat Plate in an Electrolyte,” Appl. Magnetohydrodynamics, Trudy Inst. Fis. AN Latv. SSR, Vol. 12, pp. 143–146.
4. Hamilton II, H. H., Millman, D. R., and Greendyke, R. B., 1992, “Finite-Difference Solution for Laminar or Turbulent Boundary Layer Flow Over Axisymmetric Bodies with Ideal Gas, CF4 or Equilibrium Air Chemistry,” NASA Langley Research Center report no. L-17102.
5. Henoch C. , and StaceJ., 1995, “Experimental Investigation of a Salt Water Turbulent Boundary Layer Modified by an Applied Streamwise Magnetohydrodynamic Body Force,” Physics of Fluids, Vol. 7, pp. 1371–1383.
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