This pack contains the main topics in compressible flow with elaborate explanations to concepts such as normal and oblique shocks, expansion waves, Rayleigh and Fanno Flow, as well as the one dimensional sod shock tube problem. Working MATLAB codes are also provided for the user to explore the appl...
[Show more]
1x sold
This report elaborates on some applications of oblique shocks and expansion wave relations (shock expansion theory) to calculate the drag force on a diamond airfoil at different angles of attack and solve for the flow deflection angle at the tail of an infinitely thin plate. The report also shows a ...
Preview 4 out of 33 pages
Add to cartThis report elaborates on some applications of oblique shocks and expansion wave relations (shock expansion theory) to calculate the drag force on a diamond airfoil at different angles of attack and solve for the flow deflection angle at the tail of an infinitely thin plate. The report also shows a ...
This report first explores the use of normal shock relations to determine the effect of Mach number ahead of the shock on flow properties in the form of their ratios. The report tackles property ratios such as the pressure ratio, temperature ratio, total pressure ratio, and even the Mach number behi...
Preview 4 out of 31 pages
Add to cartThis report first explores the use of normal shock relations to determine the effect of Mach number ahead of the shock on flow properties in the form of their ratios. The report tackles property ratios such as the pressure ratio, temperature ratio, total pressure ratio, and even the Mach number behi...
This report describes how a MATLAB code was used to analytically solve for flow property distributions within a one-dimensional shock tube at t=0.2s, given known initial conditions. Property distributions such as pressure and density were found to decrease with the rarefaction wave from the head to ...
Preview 5 out of 27 pages
Add to cartThis report describes how a MATLAB code was used to analytically solve for flow property distributions within a one-dimensional shock tube at t=0.2s, given known initial conditions. Property distributions such as pressure and density were found to decrease with the rarefaction wave from the head to ...
This report describes how a MATLAB code was used to analytically solve for flow property distributions within a one-dimensional shock tube at t=0.2s, given known initial conditions. Property distributions such as pressure and density were found to decrease with the rarefaction wave from the head to ...
Preview 3 out of 17 pages
Add to cartThis report describes how a MATLAB code was used to analytically solve for flow property distributions within a one-dimensional shock tube at t=0.2s, given known initial conditions. Property distributions such as pressure and density were found to decrease with the rarefaction wave from the head to ...
Stuvia customers have reviewed more than 700,000 summaries. This how you know that you are buying the best documents.
You can quickly pay through credit card or Stuvia-credit for the summaries. There is no membership needed.
Your fellow students write the study notes themselves, which is why the documents are always reliable and up-to-date. This ensures you quickly get to the core!
You get a PDF, available immediately after your purchase. The purchased document is accessible anytime, anywhere and indefinitely through your profile.
Our satisfaction guarantee ensures that you always find a study document that suits you well. You fill out a form, and our customer service team takes care of the rest.
Stuvia is a marketplace, so you are not buying this document from us, but from seller abrahamadu-mills. Stuvia facilitates payment to the seller.
No, you only buy these notes for $25.49. You're not tied to anything after your purchase.
4.6 stars on Google & Trustpilot (+1000 reviews)
67096 documents were sold in the last 30 days
Founded in 2010, the go-to place to buy study notes for 14 years now
