Boundary Layer at a Stagnation Point with Hydrogen Injection
- 1 November 1970
- journal article
- research article
- Published by Taylor & Francis in Combustion Science and Technology
- Vol. 2 (2) , 131-144
- https://doi.org/10.1080/00102207008952241
Abstract
The development of a diffusion flame at a stagnation point when hydrogen is injected into the hot on coming air flow is studied by treating finite rate chemistry for several sets of flow conditions. The limiting cases of frozen and equilibrium behaviour are presented. Relatively accurate descriptions of the chemical steps, and the thermodynamic and transport properties of the species are employed.Keywords
This publication has 10 references indexed in Scilit:
- Stagnation Point Flow with Complex CompositionPhysics of Fluids, 1968
- A finite-difference solution of similar nonequilibrium boundary layers.AIAA Journal, 1967
- Laminar Boundary Layer with Complex CompositionPhysics of Fluids, 1967
- Nonequilibrium anomalies in the development of diffusion flames.AIAA Journal, 1966
- Sublimation of graphite at hypersonic speedsAIAA Journal, 1965
- Ignition and extinction in combustion of initially unmixed reactantsJournal of Fluid Mechanics, 1965
- Laminar boundary layer with hydrogen injection including multicomponent diffusionAIAA Journal, 1964
- Application of quasilinearization to boundary- layer equationsAIAA Journal, 1964
- Calculation of Reaction Profiles behind Steady-State Shock Waves. I. Application to Detonation WavesThe Journal of Chemical Physics, 1958
- Theory of Stagnation Point Heat Transfer in Dissociated AirJournal of the Aerospace Sciences, 1958