Turbulent Boundary-Layer Heat Transfer from Rapidly Accelerating Flow of Rocket Combustion Gases and of Heated Air
- 1 January 1965
- book chapter
- Published by Elsevier
Abstract
No abstract availableThis publication has 16 references indexed in Scilit:
- Laminar Flow Heat Transfer to a Gas With Large Temperature DifferencesJournal of Heat Transfer, 1963
- A Comparison of Analytical and Experimental Local Heat Fluxes in Liquid-Propellant Rocket Thrust ChambersJournal of Heat Transfer, 1962
- Heat transfer in nozzlesChemical Engineering Science, 1959
- Convective heat transfer from hightemperature air inside a tubeAIChE Journal, 1958
- Theory of Stagnation Point Heat Transfer in Dissociated AirJournal of the Aerospace Sciences, 1958
- Heat Transfer to an Incompressible Turbulent Boundary Layer and Estimation of Heat-Transfer Coefficients at Supersonic Nozzle ThroatsJournal of the Aeronautical Sciences, 1956
- Experimental Investigation of Turbulent Boundary Layers in Hypersonic FlowJournal of the Aeronautical Sciences, 1955
- The Compressible Boundary LayerJournal of the Aeronautical Sciences, 1952
- Turbulent Boundary Layer in Compressible FluidsJournal of the Aeronautical Sciences, 1951
- Calculation of Gas Mixture Viscosities.Industrial & Engineering Chemistry, 1949