Numerical-perturbation technique for stability of flat-plate boundary layers with suction
- 1 February 1986
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 24 (2) , 208-214
- https://doi.org/10.2514/3.9247
Abstract
No abstract availableKeywords
This publication has 11 references indexed in Scilit:
- Experiments on the stability of the flat-plate boundary layer with suctionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Triple-deck solutions for subsonic flow past hymps, steps, concave or convex corners and wedged trailing edgesComputers & Fluids, 1982
- Flow over plates with suction through porous stripsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Analysis of Two-Dimensional Interactions Between Shock Waves and Boundary LayersAnnual Review of Fluid Mechanics, 1980
- Viscous Flow Drag ReductionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Computational Solution of Linear Two-Point Boundary Value Problems via OrthonormalizationSIAM Journal on Numerical Analysis, 1977
- Multistructured Boundary Layers on Flat Plates and Related BodiesPublished by Elsevier ,1974
- Determination of spatial amplification factors and their applicationto predicting transitionAIAA Journal, 1970
- Boundary-Layer Flow Near the Trailing Edge of a Flat PlateSIAM Journal on Applied Mathematics, 1970
- Self-induced separationProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1969