Abstract
An initial value method is applied for investigating laminar compressible boundary layers created by the passage of a plane shock wave over an infinite flat plate. The two point boundary value problem is reduced to an initial value problem by using the theory of transformation groups and is then integrated by Runge-Kutta-Gill method. The advantages of this method over the methods employed usually are that it gives good results without initial guesses and iterative processes and it is simple and direct both in concept and in application.
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.