SECOND-ORDER EFFECTS IN LAMINAR BOUNDARY LAYERS
- 1 January 1963
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 1 (1) , 33-40
- https://doi.org/10.2514/3.1462
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
- STAGNATION POINT FLOW OF A VARIABLE PROPERTY FLUID AT LOW REYNOLDS NUMBERSPublished by Defense Technical Information Center (DTIC) ,1962
- The boundary layer on a flat plate in a stream with uniform shearJournal of Fluid Mechanics, 1961
- Vorticity Interaction at an Axisymmetric Stagnation Point in a Viscous Incompressible FluidJournal of the Aerospace Sciences, 1959
- Vorticity Effect on the Stagnation-Point Flow of a Viscous Incompressible FluidJournal of the Aerospace Sciences, 1959
- The Viscous Flow Near a Stagnation Point When the External Flow Has Uniform VorticityJournal of the Aerospace Sciences, 1959
- The Transverse Curvature Effect in Compressible Axially Symmetric Laminar Boundary-Layer FlowJournal of the Aeronautical Sciences, 1956
- Viscous Flow Along a Flat Plate Moving at High Supersonic SpeedsJournal of the Aeronautical Sciences, 1956
- Readers ForumJournal of the Aeronautical Sciences, 1955
- The role of coordinate systems in boundary-layer theoryZeitschrift für angewandte Mathematik und Physik, 1954
- On the Flow of an Incompressible Viscous Fluid Past a Flat Plate at Moderate Reynolds NumbersJournal of Mathematics and Physics, 1953