Laminar Heat Transfer Over Blunt-Nosed Bodies at Hypersonic Flight Speeds
- 1 April 1956
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Jet Propulsion
- Vol. 26 (4) , 259-269
- https://doi.org/10.2514/8.6977
Abstract
No abstract availableKeywords
This publication has 11 references indexed in Scilit:
- Effect of Large Temperature Changes (including Viscous Heating) Upon Laminar Boundary Layers with Variable Free-Stream VelocityJournal of the Aeronautical Sciences, 1954
- Note on the Prandtl Number for Dissociated AirJournal of the Aeronautical Sciences, 1953
- The Effect of Dissociation in the Stagnation Region of a Blunt-Nosed BodyJournal of the Aeronautical Sciences, 1953
- On the Boundary-Layer Equations in Hypersonic Flow and Their Approximate SolutionsJournal of the Aeronautical Sciences, 1953
- A Solution of the Laminar Boundary-Layer Equations for a Compressible Fluid with Variable Properties, Including DissociationJournal of the Aeronautical Sciences, 1952
- Quantentheorie des N2-MolekülsZeitschrift für Naturforschung A, 1952
- Correlated incompressible and compressible boundary layersProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1949
- Steady flow in the laminar boundary layer of a gasProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1949
- Approximate Calculation of the Laminar Boundary LayerAeronautical Quarterly, 1949
- Temperature and Velocity Profiles in the Compressible Laminar Boundary Layer with Arbitrary Distribution of Surface TemperatureJournal of the Aeronautical Sciences, 1949