Abstract
The laminar diffusion and combustion of a gas injected into a high-speed uniform stream by means of a wall slot are considered. The Dorodnitzin-Howarth transformation is employed to reduce the boundary layer equations to incompressible form; the nonsimilar flow field is treated by a modified Oseen approximation in conjunction with the integral method. Thermal boundary conditions corresponding to an adiabatic wall and to constant wall enthalpy are discussed. The injection of homogeneous, heterogeneous, nonreactive, and reactive gases is treated. For the latter case, the models usually employed for chemical behavior, namely, frozen and equilibrium flow, are considered. The analysis is applicable to a wide variety of laminar flows, e.g., those involving cooling, thermal protection, skin-friction reduction, and supersonic deflagration. A numerical example of practical interest in connection with the venting of gaseous hydrogen boiloff from a rocket booster is presented.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.