Concentrated vortex on the nose of an inclined body of revolution
- 1 May 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 14 (5) , 698-700
- https://doi.org/10.2514/3.7145
Abstract
No abstract availableThis publication has 14 references indexed in Scilit:
- The turbulent boundary layer with foreign gas injection—I. Measurements in zero pressure gradientInternational Journal of Heat and Mass Transfer, 1974
- Prediction of Transpired Turbulent Boundary LayersJournal of Heat Transfer, 1974
- Kinematic eddy viscosity at low Reynolds numbers.AIAA Journal, 1973
- A note on von Kármán's constant in low Reynolds number turbulent flowsJournal of Fluid Mechanics, 1972
- Calculation of Compressible Turbulent Boundary Layers with Heat and Mass TransferAIAA Journal, 1971
- On a calculation method for compressible turbulent boundary layer flows with heat transferPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1971
- Characteristics of turbulent boundary layers at low Reynolds numbers with and without transpirationJournal of Fluid Mechanics, 1970
- The constant property turbulent boundary layer with injection; A reanalysis of some experimental resultsInternational Journal of Heat and Mass Transfer, 1970
- On a finite-difference solution for the constant-property turbulent boundary layer.AIAA Journal, 1969
- Transition Studies and Skin-Friction Measurements on an Insulated Flat Plate at a Mach Number of 5.8Journal of the Aeronautical Sciences, 1956