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- 1 December 1957
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 24 (12), 911-925
- https://doi.org/10.2514/8.3999
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- Transient Temperature Distributions and Thermal Stresses in Fuselage Shells with Bulkheads or FramesJournal of the Royal Aeronautical Society, 1956
- On Asymptotic Solutions for the Heat Transfer at Varying Wall Temperatures in a Laminar Boundary Layer with Hartree's Velocity ProfilesJournal of the Aeronautical Sciences, 1953
- Heat Transfer to Constant-Property Laminar Boundary-Layer Flows with Power-Function Free-Stream Velocity and Wall-Temperature VariationJournal of the Aeronautical Sciences, 1952
- Calculation of the Thermal Boundary Layer of a Body in Incompressible Laminar FlowJournal of the Aeronautical Sciences, 1951
- Contributions to the theory of heat transfer through a laminar boundary layerProceedings of the Royal Society of London. Series A - Mathematical and Physical Sciences, 1950
- Temperature and Velocity Profiles in the Compressible Laminar Boundary Layer with Arbitrary Distribution of Surface TemperatureJournal of the Aeronautical Sciences, 1949
- The Aerodynamic Forces on an Oscillating Airfoil at Supersonic SpeedsJournal of the Aeronautical Sciences, 1947